NOTE: Please replace this service manual with the old DP-1100's manual (B51-1592-00). This manual has all descriptions for DP-1100 and DP-1100II.
DANGER: Laser radiation when open and Interlock defeated. AVOID DIRECT EXPOSURE TO BEAM.
.
FOKG: Refer to "IC15 pin function" on page 69.
An analog voltage is continuous in respect to time, and has a value at each time of t1, t2, t3, etc. as shown in Fig. 1.1 and as well a value at any time between t1 and t2.
If an analog voltage is represented corresponding to a code system, the analog voltage over the definite time range of t1 to t2 is made of the indefinite number of codes. In order to transmit a digital signal corresponding to the voltage at t1, it needs a definite time length, but when transmitting indefinite codes, the transmission does not end forever.
Therefore, in case where an analog voltage is converted to a coded system, analog voltages at timings with some interval are only converted as shown in Fig. 1.2. With such a process, the definite number of codes corresponding to the definite timings, for example, five codes for the time interval t1 to t5 are produced.
When having transmitted codes described in Fig. 1.2, only five codes can be received at the receive side between t1 and t5. The number of voltage values reproduced thereby is only five, any voltage at timings except t1, t2, t3, etc. cannot be determined.
However, if the frequency component (20 kHz) of the original analog signal is less than the value (44.1 kHz) depending upon the time interval between timings t1, t2, t3, etc. at which coding is staged, even the value for non-transmitted portions can be reproduced. To pick up analog values at a fixed time interval by such a process is called "sampling".
Fig. 1.3 indicates one example where analog signals ranging from OV to 10V are converted to 11-step voltage values of OV, 1V, 2V,...,9V and 10V via round-off. With this conversion, preparation of only 11 kinds of codes is needed. To convert an analog signal to a kind of a digital signal with the process of round-off or the like is called "Quantization".
Fig. 1.4
1-3 SAMPLING THEOREM
The frequency of picking up an analog signal, for example, 50,000 times per second, is called "a sampling frequency. It is proven that if sampling is conducted at the rate larger than a certain value, the original waveform can be reproduced just the same to an inch. This is called "a sampling theorem".
Sampling Theorem: If sampling is conducted at the frequency (44.1 kHz) which is over double the maximum frequency (20 kHz) in a spectrum of a signal, the original waveform can be completely reproduced.
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A rounding error is caused by quantization at sampling points as described in 1-2, and seeing Fig. 1.6 it can be thought that this rounding error is created as a distortion or noise. This
noise is of the nature different from noises emitted from an analog system, being called "a quantization noise".
The ratio of a quantizing noise against the maximum value of the signal in a binary-coded 16-bit system is plotted in respect to a sinusoidal wave input as shown in Fig. 1.7.
If a 16-bit code is used in quantizing one sampled value, the number of steps which can be taken, i.e., the quantizing number N is given as follows:
N = 216 = 65536
When making the amplitude of 0 to V corresponding to this, the width E0 of one quantization step is given by:
Therefore, the amplitude of a quantizing noise is E0 at the peak-to-peak value, so that the noise power N2 is:
On the other hand, supposing that an input signal is a sinusoidal wave whose amplitude at the peak-to-peak value is V, the signal power S is:
To convert a level of an analog signal at every interval of a fixed period (1/44.1 kHz = 22.7 µs), as described in 1-4, to a binary code (1 and 0) after quantization is called a "PCM" (Pulse Code Modulation).
PCM has various kinds of modulation systems, but here a Sony and Philips jointly developed new system, called EFM, used for DAD is described.
Therefore, the power ratio is:
The purpose of the margin bits is to reduce a DC component and low frequency components by adding three additional bits to the signals converted into EFM.
One of 14 bits converted from 8 bits is called a channel bit.
(1) EFM is the modulation to first divide a 16-bit datum (data bit) into two 8-bit data and then convert each of these 8-bit data to a 14-bit datum (channel bit) as shown in Fig. 1.8. The conversion is to select patterns of 28 kinds among patterns of 214 kinds, meeting the following condition. Channel bits of 28 meeting this condition have been predetermined by a computer as indicated in Tables 1-1 and 1-2:
Two or more but 10 or less 0s (zeros) should be always inserted between channel bits 1 and 14.
(2) Three channel bits are always inserted between 14-bit blocks. The role of these 3 bits is to make adjustment so that the above condition (enclosed in the box) is met even at the connection of blocks.
8 bit | s→14 bits | ||||
---|---|---|---|---|---|
Order | data bits | channel bits | |||
0
1 2 3 4 5 6 7 8 9 10 11 2 3 4 5 6 7 8 9 10 11 2 3 4 5 6 7 8 9 10 11 2 13 14 5 16 17 8 9 0 11 2 2 2 3 4 5 6 7 8 9 10 11 2 2 2 3 4 5 5 6 7 8 9 10 11 2 2 2 3 4 5 5 6 7 8 9 10 11 2 2 2 3 4 2 5 2 2 3 3 3 3 3 3 3 3 3 3 3 3 3 |
|||||
♥ d1d8 |
★ ↓
C1C14 |
||||
8 bits⊶14 bits | ||||||||
---|---|---|---|---|---|---|---|---|
Order | data bits | channel bits | ||||||
64
65 667 688 69 70 71 723 74 75 76 77 78 79 80 81 82 83 84 85 88 90 91 92 93 94 95 96 97 98 90 101 1023 104 105 106 107 1023 114 115 116 117 122 123 124 126 |
01000000
01000001 0100001 0100001 0100001 01000101 01000101 01000101 010010 |
|||||||
L | 127 | 01111111 | 00100000000010 |
EFM Conversion table 0 to 127 (NRZ-1 represantation)
8 | bits→14 bits | |
---|---|---|
Order | data bits | channel bits |
128
129 130 131 132 1334 1356 137 1389 140 142 143 145 147 143 1445 1457 1534 1557 1556 15789 161 1623 1667 1667 1667 1773 1756 1777 1789 1881 1883 1885 18890 191 |
||
▼ C1 C14 |
C1 | is | first | cut |
---|---|---|---|
13 | mat | cut. |
EFM Conversion table 128 to 255 (NRZ-1 representation)
cf: NRZ Non Return to Zero
8 bi | ts→14 bits | |
Order | data bits | channel bits |
192
193 194 1956 197 198 200 202 203 204 205 206 207 208 210 211 212 213 214 215 2167 218 219 2203 221 212 214 215 2223 2224 2226 2227 2228 2229 231 232 2334 235 66 237 238 239 240 241 243 244 245 244 245 244 245 |
11000000
1100001 1100001 1100001 1100010 1100010 1100010 1100010 1100010 1100100 |
|
247
248 249 250 251 252 |
11110111
1111000 11111001 1111010 11111010 11111011 111111 |
00100010010010
01001000010010 100000000 |
253
254 255 |
00001000010010
00010000010010 0010000001001 |
data bits
channel bits
Reproduction signals cannot be recovered RF signals do not come out for a long time due to dropout or one information bit has been shifted owing to jittering in digital recording or playback. Because one bit shift of a digital signal makes the signal quite different in its signal level.
Therefore, by dividing a recorded signal to many small blocks, the system is organized so that even when a signal is disturbed due to jittering or the like, a bit synchronization is always estabilished at the new block to identify the joint part between blocks. Such a block is called a ''Frame''. Frame Sync signals are inserted to indicate the boundary of the frame and to make a bit synchronization. Fig. 1.9 shows the structure of one frame.
Channel bits | Margin bits | Total bits | ||
---|---|---|---|---|
Frame Synchro-
nization |
24 | 3 | 27 | |
Users buts | 14 | 3 | 17 | |
Data bits | 14 bit x 24 = 336 |
3
bit × 8 = 24 = 72 |
408 | |
Error correction bits (Parity bits) | 14 bit×8=112 | 3 bit x 24 | 136 | |
486 | 102 | 588 |
Fig. 1.9
moisture absorption causing bend is a big defect. (Refer to precautions on handling the disc.)
Fig. 1-11
Fig. 1.12
Lead In: TOC (table of contents) → Absolute time of the heading of music is included. Lead Out: Used for retrieving of the heading indicates of program end. Other → Control Data P, Q
11.
12. Double Refraction
The rating of double refraction is represented by a light path difference (mm). Rating: 100 mm
The main cause of double refraction is mold distortion. Fig. 1.14
Fig. 1.14
13. CD is tough against dusts Fig. 1.15(a) and (b)
(a) In a case where dusts are deposited on the disc surface
14. Fabricating process of baseplate. Fig. 1.16
Fig. 1.16 Manufacturing Process of CD
Fig. 1.17 Encoding system
Even if reading every page of a book slantwise from its upper left side to lower right side, you can fully recognize the context or contents. However, you cannot recognize the contents of the book if you are reading carefully one character or clause without reading several tens of pages.
An error collection code is the same as this, and correction is easy even when code errors of some bits are present. However, if many, say 1000, bits are consecutively wrong at a time, it is very difficult to correct those errors.
Therefore, the technique with which an order of a signal is once changed and then recorded and, after reproduction, returned back to the original order is employed. This changing of the order of a signal is called an "interleave", and the returning to the original order is called a "deinterleave".
Fig. 2.1 is the illustration explaining the principle of interleave. The order of a signal at fabrication of the disc is out of order. Therefore, by deinterleaving the signal, successive code errors are disperesed, so that operation of error correction and associated jobs are made facilitative.
Signal words returned to their original locations (10 successive error words are dispersed.)
Fig. 2.1
(4) Bill (d) illustrates the example that the location to be corrected is known, and the correction can be done by the same means as in bill (b). The means to indicate the location of error in such a way is called a "pointer".
In the examples of (1) to (4), "Total P" is used for check of error or erasure of data A, B, C and D. A word used for check and correction besides required data is called a "parity word" or a "parity bit".
Syndrome (Checking) S=A+B+C+D-P=0
Bil | ll (b) | ||||
---|---|---|---|---|---|
+ |
A'
B* C' D' |
¥
¥ ¥ ¥ |
100
? 300 400 |
◄ Disppearan | |
Tota | al P' | ¥ | 1,000 |
Syndrome (Checking) S = A' + B' + C' + D' - P = 0 B = B* - S = 200
Bill (c) | ||||
---|---|---|---|---|
A' | ¥ | 100 | ||
Bʻ | ¥ | 300 | ||
C' | ¥ | 300 | ||
+ | D' | ¥ | 400 | |
Tota | al P' | ¥ | 1,000 |
S = A' + B' + C' + D' - P' = 0
Bill (c | 4) | |||
A' | ¥ | 100 | ||
В* | ¥ | 300 | ||
C' | ¥ | 300 | ||
+ | D' | ¥ | 400 | |
Tot | al P' | ¥ | 1,000 | - |
S = A' + B' + C' + D' - P' = 100 B = B* - S = 200
(1) In case of (3) in 2-4, correction is infeasible because the location of error is unknown. Even in such a case, the way by which correction is feasible is a single error correcting method. In 2-4, there is only one parity word, P. Besides this, a "Weighted Total Value", Q, is used. Because two parity words P and Q are used, there are also two syndromes S1 And S2.
Now suppose that there is an incorrect bill (b) in respect to a correct bill (b) and that the location of error (one) in bill (b) is unknown.
Supposing that the differences from original values are EA, EB, EC, ED, EP and EQ with respect to A', B', C', D', P' and Q', respectively, of bill (b) (for no error, EA, to EQ=0) A' = A + EA, B' = B + EB, C' = C + EC, D' = D + ED, P' = P + ED, Q' = Q + EQ
Obtaining syndrome S1,
S1 = A' + B' + C' + D' - P' = (A + EA) + (B + EB) + (C + EC) + (D + ED) - (P + EP) = A + B + C + D - P + EA + EB + EC + ED - EP - EP - (1) 0 = EA + EB + EC + ED - EP
Obtaining syndrome S2
S2 = 4A' + 3B' + 2C' + D' - Q' = 4A + 3B + 2C + D - Q + (4EA + 3EE + 2Ec + ED - EQ) (2) 0 = 4EA + 3EB + 2Ec + ED - EQ
Supposing that a code error is one word between A' to P', Q'
(1) | A' wrong | S 1 = E A , S 2 = 4E A |
---|---|---|
(11) | B' wrong | S 1 = E B , S 2 = 3E B |
(111) | C' wrong | S 1 = E c , S 2 = 2E c |
(IV) | D' wrong | S 1 = E D , S 2 = E D |
(VI) | P' wrong | S 1 = E P , S 2 = 0 |
(VII) | Q' wrong | S 1 =0, S 2 =-E 2 |
By a method where two syndromes are introduced as mentioned above and determined, wrong words can be found and corrected.
Bill (a) | |||||||
А | ¥ | 100 | |||||
В | ¥ | 200 | |||||
С | ¥ | 300 | |||||
D | ¥ | 400 | |||||
Ρ | ¥ | 1,000 | |||||
Q | ¥ | 1,000 | |||||
P=A+B | + C | + D | |||||
Q = 4A + | Q = 4A + 3B + 2C + D | ||||||
- |
Syndromes S1 = A + B + C + D - P = 0 S2 = 4A + 3B + 2C + D - Q = 0
and the second | |||
---|---|---|---|
Bill (b) | |||
A' | ¥ | 100 | |
Β′ | ¥ | 300 | |
C′ | ¥ | 300 | |
D' | ¥ | 400 | |
Ρ | ¥ | 1,000 | |
Qʻ | ¥ | 2,000 | |
Syndrome
S1=A'+B'+C'+D'-P'=100 S2=4A'+3B'+2C'+D'-O'=300
(2) The principle of double erasure correction is described below. In this case, the location of error is indicated with a pointer. It is here known that two words in bill (c) are wrong and there are no other wrong words. Using equation (1) in paragraph (1).
O
Supposing EA = 0, ED = 0 and EP = 0
S1=EB+Ec=200 _____(3)
From Equation (2) of (1)
S2 = 4A + 3B + 2C + D + (4EA + 3EB + 2Ec + Ep - EQ) = 500
S2 = 3EB + 2EC = 500 _____ (4)
Determining EB and Ec from simultaneous equations of (3) and (4),
EB = 100 | |||||||
---|---|---|---|---|---|---|---|
Bill (c) | |||||||
A' | ¥ | 100 | |||||
B' | ¥ | 300 | |||||
Cʻ | ¥ | 400 | |||||
D' | ¥ | 400 | |||||
P' | ¥ | 1,000 | |||||
Q' | ¥ | 2,000 | |||||
Pointer
Ec=100
S1=A' + B* + C* + D' - P' = 200 S2 = 4A' + 3B' + 2C* + D' - Q' = 500 Where B* = E + EB C* + = C + Ec
This theory is the principle of a Reed Solomon Code. In practice, the Reed Solomon Code with four parity words is used.
(1) Fig. 2.2 shows a principle of a cross-interleave. An original series of signals is divided into a number of words, and parity words are inserted.
(5)
Four original series of signals (W1, W5, W9, W13...), (W2, W6, W10, W14,...), (W3, W7, W11, W15,...) and (W4, W8, W12, W16,...) among many original series of signals are arranged for four lines No. 1 via No. 4 in Fig. 2.2 of these words, the words passing through No. 1 are
delivered directly, but words fed into No. 2 to No. 4 lines are subject to delay with delay memories by one to three words so that the word order is changed (interleaved) at their respective terminals.
There is an adder following the delay memories, where another parity word Q is created.
(6)
In other words, two system of codes are used on both sides of the delay memories.
(2) Fig. 2.3 indicates relations between two parity codes. The solid lines mean a P's series, and the dotted lines mean a Q's series. Each of them has the capability of single erasure correction, so that an error of a single word can be easily corrected of course.
The | syndrome | of eac | h othe | 's | series | can | be | used | as | а | |
---|---|---|---|---|---|---|---|---|---|---|---|
pointer for pointing out a location of error. |
Fig. 2.3 Code Series of Cross Interleave (Black circules indicate errors).
A pickup part corresponding to a cartridge for a conventional analog player is detailed later. Briefly speaking, this part allows the laser diode to emit a light beam (\u03c6 = 780 nm) and convert the intensity of the reflected light from disc pits into electric signals.
A signal detected at a pickup is delivered to a signal processing circuit, and split into the following three signals.
A focus error signal is fed into a focus servo circuit to control a lens system with the use of a focus servo coil (like a voice coil of a loudspeaker) so that the focus spot of the laser beam is
always kept on a pit surface against fluctuations due to the revolutions of a disc. (The same as auto-focusing in an EE camera)
Because a compact disc has no guide groove, it is needed to operate a servo so that a laser beam spot can automaitcally follow a signal track. A tracking error signal is fed into a track-
ing servo circuit, the output of which drives a tracking servo coil to operate the servo system.
24
Constant linear velocity (CLV) means to keep a line speed at a constant speed of approx. 1.2 m/sec.
For this purpose disc is rotated: approx. 500 r.p.m. at inside
radios approx. 200 r.p.m. at outside radios
The CLV servo circuit is the circuit to servo-control revolutions of the disc motor to keep circumferential speed of the disc constant.
The RF signal is being delivered from the signal processing circuit as described under 3-2. The RF signal is vaired acording to appearance or disappearance of a pit on a disc. This signal can be displayed on an oscilloscope as illustrated in the Fig. 3-5.
The waveform is generally called "Eye Pattern".
Fig. 3-5 is sketches explaining concept of the eye pattern. The RF signal is converted to a digital signal composed of 1s and 0s with the aid of a comparator to generate an EFM signal.
Fig. 3.5
A LED is formed with a P-N junction composed of an n-type semiconductor which allows electric conduction with electrons and p-type semiconductor in which holes serves electric conduction. Applying a voltage in the forward direction, electrons in the n-type semiconductor are injected into the p-type semiconductor, and holes in the p- type semiconductor are injected into the n-type semiconductor. Red luminescence is emitted when electrons injected into the p-type semiconductor tor combine with holes.
Green luminescence is emitted when holes injected into the n-type semiconductor combine with electrons.
Fig. 4.1
A laser diode, as mentioned 4-1 , is the same as an LED in terms of recombination luminescence of carriers, but different in that the light emitted is a coherent laser light, the phase of which is uniform (single wavelength).
(1) Oscillation Wavelength
According to a CD's proposal, there should be the following relaiton between a wavelength of a laser diode and the number of aperture of lens NA: λ/NA = 1.75 μm
As long as today's GaAlAs material is used, it is difficult to make a laser diode having a wavelength shorter than apporx. 760 nm, but a laser diode with higher than 780 nm can be made in mass production.
Therefore, NA = λ/1.75 μm = 0.446
As the result, the objective lens in the pickup used in DP-1100B/II has been designed for approx. NA = 0.47 ± 0.01
An laser diode has a threshold current I, with which oscillation starts, and with a current larger than this threshold level, a light power P increases linearly with increase of a current I. Furthermore, if keeping drive at a fixed current, the light outpout is greatly varied due to temperature increase. Therefore, control is always done so that the light output is kept constant.
Fig. 4.2 Oscillating Characteristic of a Laser Diode
Light beams emitted from a semiconductor laser are changed to parallel light ralys by a collimator lens system and enter a polarization prism. Since the semiconductor laser beams are linear-polarized in the direction vertical to the plane of incidence, the beams are reflected by the polarizing film. The light beams reflected from another plane of the polarization prism pass through a quarter-wave plate, and then are converged to a spot of nearly 1.5 µm in diameter with the aid of an objective lens.
The light reflected from a disc passes again through the objective lens and follows the same path as the forward path to the polarizing film. By the effect of the quarter-wave plate, the light incoming into the polarizing film is changed so that its polarizing direction is perpendicular to the polarizing direction in the forward path. Therefore, the light transmits the polarizing film and does not go back to the semiconductor laser. Next, the light incoming into a critical angle prism for detection of a foucs point is reflected three times inside the prism and then fed into 4-divided photodiodes. The output of these photodiodes are used for controling a tracking servo coil and a focus servo coil to obtain an optimum focusing of the abjective lens on pits of the disc.
Diffused light beams are changed to parallel light beams. Light beams distributed in oval pattern is changed to approx. circular distributions.
(2) Polarized Prism
Light polarized in parallel to a surface is reflected, and light polarized in vertical is passed through the prism.
(3) 1/4 Wavelength Plate
(4) Objective Lens
(5) 4-divided photodiodesConverts light into an electrical signal.
To read tiny pits (width: 0.5µm, length 0.9#3.2 µm) on a disc by means of a laser spot, the location must be precisely controlled to follow surface and axial deviations of the disc caused by rotating the disc for playback. For this purpose,
must be detected. The detection muthods for both errors will be given below.
When a light beam is passed from a high refraction material to a low refraction material, a relaion, as shown in Fig. 5.2, is existed between the incident angle and refleciton ratio at the boundary of the materials. As can be seen from the graphs, the reflection ratio will change rapidly as the incident light angle changes in the area where the incident angle is slightly less than the critical angle.
Fig. 5.2 Refleciton changes rapidly at angles dose to critical angle.
In Fig. 5.3, the angle of the critical prism has been adjusted so that the incident light angle is just equal to the critical angle for a center light beam of incident light. Accordingly, if parallel light beams are impinged, the incident light angle is equal to critical angle for all light beams and all light beams are reflected, giving equal light amount to each element of 4-divided photo-diodes (PDa, PDb, PDc and PDd). If diffused or divergent light is impinged, reflection strength at a left half of the prism lowers and light amount received by the photo diodes PDa and PDb will be decreased. On the contrary, if convergent light is impinged, light amount received by PDc and PDd is reduced. By utilizing this phenomenon, the photo diodes convert light received into four electrical signals and the signals are processed with a differential amplifier to provide a focus error signal in terms of (A1 + A2) – (A3 + A4).
(A1, A2, A3, and A4 Are electrical signals developed by PDa, PDb. PDc and PDd. respectively.)
Fig. 5.4 Focus error detection method using a critical angla prism
Tracking error is a deviation of the reading light spot from the pits (track) to be traced.
In the Pickup a method called "heterodyne system" is adopted to detect the spot deviation from a pit.
The heterodyne system is based upon the distribution of the reflected light diffracted from a pit depends upon a relative location of the pit and spot.
In this system, each electrical signal converted by the 4-divided photodiode is assumed as A1, A2, A3 And A4, and A1+A3 and A2+A Are evaluated. Namely, both phases for A1+A3 and A2+A4 are the same when the tracking is established, while phase difference will be caused when the spot deviates from a pit.
A RF signal is a sum of each electrical signal A1, A2, A3 and A4 developed by the 4-divided photodiode (refer to 3-5). The RF signal is then processed to provide EFM signal. The EFM signal is then converted into an analog signal in passing through a D-A convertor after demodulated.
When the LDC goes H, the output of TA75458(Q108) becomes positive as shown in the schematic diagram, And a current flowing through R145, D102, And D104 turns Q109 cut off, thereby stops the oscillation of the Laser Diode.
When the LDC goes to L level, the output of TA75458 (1/2) changes to negative, and this allows bias current of Q109 to flow from its emitter to the base, thus Q109 is turned on and the Laser diode emits infrared light (810 mm).
When light emitted from the laser diode is impinged to the pin diode, a current proportional to strength of the light flows from anode to cathode of the diode. With the strength of the light increased, a voltage developed across R113 also increases and makes non-inverted (+) terminal of the operational amplifier positive. As the result, the operational amplifier output also increases in positive, thus reducing the current flowing into the laser diode.
1) Address Data (Q Signal) Reading Section
In the CD system specifications, one symbol consisting of 8 bits and located after frame synchronization signal of PCM data is called CONTROL & DISPLAY SYMBOL, and each of 8 bits is called P-Channel, Q-Channel,
R-Channel....& W-Channel. Of the eight channels, Q-Channel is used for address data and one address data is comprized of 98 frame Q-Channel data. Fig. 5.6 shows this configuration of the CONTROL & DISPLAY symbol data.
Fig. 6-1
Address data format (outside lead-in area) are as follows:
CONTROL: 4 bits control data, MSB indicates pre-emphasis on or off, and LSB indicates 4CH/2CH.
ADR: | 4 bit mode data | |||||||||
---|---|---|---|---|---|---|---|---|---|---|
MODE 1 (1 in BCD): Adress mode | ||||||||||
MODE 2 (2 in BCD): Disc catalog number mode | ||||||||||
MODE 3 (3 in BCD): Special information mode (recorded by alphanumeric code 0#9, A#Z) | ||||||||||
MNR: | Program number expressed by BCD in 2 digits (8 bits) | |||||||||
X: | Index for each program expressed by BCD in 2 digits (8 bits) | |||||||||
MIN: | Elapsed time (minute) for each program expressed by BCD in 2 digits (8 bits) | |||||||||
FRAME: | Elapsed time for each program expressed by BCD in 2 digits (8 gits) (Frame, 1 frame = 1/75 sec) | |||||||||
ZERO: | Not used (8 bits ødata) | |||||||||
A MIN: | Elapsed time (sec) for disc expressed by BCD in 2 digits (8 bits) | |||||||||
A SEC: | Elapsed time (sec) for a disc expressed by BCD in 2 digits (8 bits) | |||||||||
A FRAME: | Elapsed time for a disc expressed by BCD in 2 digits (8 bits) (frame). | |||||||||
CRC: | 16 bit CRC code data calculated for data CONTROL #A FRAME. |
Each figure under a code shows bit number required for the code.
S 0 , S 1 | CONTROL | A D R | MNR | x | ΜΙΝ | SEC | FRAME | ZERO | AMIN | ASEC | AFRAME | CRC | S 0 ,S 1 - |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
, | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 10 | |||||
2 | 4 | 4 | 8 | 8 | 8 | 8 | 8 | 8 | 8 | 8 | 8 | 16 |
Fig. 6-2 Address Data configuration
Subsequent to ''1-2 Head amp'', the servo PCB and the process PCB are described in order along the RF signal flow.
The four signals from the pickup are input to preamplifier IC (Q103) on the mechanism PCB.
The internal block diagram of Q103 is shown in section 2-1-1. Through the resistors, connected between pins 1 and 2 and between pins 15 and 16 of Q103 (TA7731P), focus balance and SVC operation (described later) are performed. Weak signal is amplified and output to servo PCB as S1 and S2.
The FE amplifier and peak detector, consisting of Q101 and Q104, is a circuit to generate the focus error signal. Peak detection is made with the B-E diode characteristic of Q104 and the CR time constant of its emitter. The focus error signal is obtained from (C + D) - (A + B) operation of the picked-up four signals from the pickup by Q101.
The servo control (SVC) is performed by processor IC12 on the process PCB (X32-1010), when the disc is exchanged or
when play mode is entered from stop mode. It checks the number of data errors to control control inputs A, B, C and INH of Q102 on the mechanism PCB to obtain the optimum playback.
The internal block diagram and truth table of Q102 is shown in Fig 2-1 C and D of section 2-1-2. Inputs A, B, C and INH, determine which output 0 to 7 (bilateral switch should be internally connected with COM).
Q105, which is the laser ON/OFF switch, turns ON with "L" signal LDC (J8-3P) from the microprocessor so that the laser diode emits light. This laser diode incorporates a light emission monitor diode. Then, APC operation is performed by using the monitor output as the APC control input.
FG signal is produced by Q101, Q108 and Q109 to monitor the rotation of the disc motor. Q101 performs amplification and Q108, Q109 and D104 perform waveform shaping. For adjustment of each trimming potentiometer, refer to "Adjustment" on page 165.
Fig. 1-1-3 SVC Circuit Operation
The focus error (FE) signal, generated in the mechanism PCB, is fed into pin 8 of CN6 on the servo PCB. This signal is used in making signal DOK which the presence or absence of the disc is judged when the tray is closed.
With a disc present, "L" signal DOK is output from pin 1 of CN2 to pin 27 of IC15 on the process PCB (X32).
On the other hand, when the RF signal from the pickup is input to pin 20 of IC15, pin 12 (FOK) of IC16 is at -12 V and O2 turns OFF. Signal FE through focus gain adjustment potentiometer VR1 is amplified in IC1 (1/2) and input to IC2 (1/2) via the phase correction CR circuit. Then, the signal power-amplified in IC2 (1/2) drives the pickup actuator coil to form a servo loop including the optical pickup by which the laser beam is always focused exactly on the disc pit surface irrespective of the amount of disc warp, etc.
During light emission of the laser diode, the gate of FET Q4 connected to the LDC line is "L" so that IC2 (1/2) performs normal amplification. In addition, the gate of Q6 connected to the FOK line is at -12 V when RF signal is provided. Therefore, Q6 turns OFF and amplification is possible in the loop connecting IC1 and IC2, where the focus servo works.
Signals S1 (A + B) and S2 (C + D), produced by the preamplifier on the mechanism PCB, are fed into pins 6 and 7 of connector CN6. These signals are partially amplified by a 3-stage amplifier of inverter IC5 to generate the tracking error signal, then waveform-shaped by IC7 and input to TS1 and TS2 of IC15.
The tracking error signal is generated in IC15 and output from TEOP and TEON. This signal works as the tracking servo signal.
On the other hand, signals S1 and S2 are combined via R100 and R101 to extract music signal. The combined signal is input to IC6 which acts as an amplifier like IC5. After 1st stageamplification, it is further 2-stage amplified through the EFM test point via the second-stage amplifier which is biascontrolled by DSV and is input to pin 17 (EFM I) of IC15.
The tracking error signals output from pins 3 and 4 of IC15 (TEOP and TEON) are combined in IC12 (1/2). The combined output (TE) is phase-inverted in IC14 (1/2) and input via tracking gain trimming potentiometer VR2 to pin 6 of IC1 (2/2) in which it is phase-corrected and amplified.
Further, output of IC1 (2/2) is power-amplified in IC2 (2/2), Q10 and Q11. Amplified TE signal drives the pickup actuator coil to form a tracking servo by which the laser beam spot follows exactly the pit sequence on the disc.
Pits are made on a disc in such a way that the sum of "H" durations is equal to that of "L" durations i.e. DSV (Digital Sum Value) is zero. Thus, this circuit controls the amplifier bias so that the data on the disc is identical to that read by the player, thereby decreasing error.
The signal from pin 4 of IC6 is further amplified and applied to the base of Q21. The variation in amplitude of the DC component, that is equivalent to the amplitude of the EFM signal wave, appears in the emitter of Q21. This DC component is amplified only in low frequency by IC8 (1/2) and applied to the gate of AGC FET Q33, thus reducing the change in EFM signal. In addition, the EFM signal is level-compared in IC10 (1/2). Then "L" at pin 1 of IC10 (1/2) informs to pins 20 (RFOK) of IC15 on SERVO (×29) PCB and 29 (RFOK) of IC15 on the process (X32) PCB through pin 1 of CN7 that the EFM signal is provided.
In addition, the EFM signal is also applied to IC10 (2/2) via diode D19 for level-comparing. Then, it is output from pin 8 as signal RFES. This signal is used in dropout control on play or used in the kick processing circuit at kick of motor.
As play advances tracing the disc pit sequence by the pickup, a positive offset voltage appears at the output of tracking coil driver pin 8 of IC2 (2/2) by the tracking servo function. Since the high-frequency component, which is also contained in the tracking driver output besides the offset voltage, is unnecessary for driving the pickup carry motor, it is eliminated by an LPF amplifier of IC3 (2/2). Further, this output is power-amplified in IC4 (2/2) to drive the pickup carry motor.
In addition, Q14 is ON to avoid application of the tracking servo output signal during modes other than play. Signal PUFB, which is entered to the input of the power amplifier (pin 3 of IC4 (2/2)), is used in kick operation or fast movement of the pickup.
When pin 15 (MSP) of IC15 on the servo PCB emits an "H" signal according to the CPU command, the gate of Q17 becomes "L" and Q17 turns OFF. Disc motor driver IC4 (1/2) can amplify signal AFC emitted from IC8 on the process PCB due to start the disc motor. Due to shorten the start time or the stop time, a circuit consisting of Q19, C36, Q18 and R94 applies positive or negative pulse to the pin 7 of IC4 (1/2). (Positive pulse at motor's start Negative pulse at motor's stop).
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1100R/11
3-state output situation in pin 9 of IC15 is used for driving the tray motor. The signal at "H" is inversion-amplified in IC3 (1/2) to drive Q16 to make pin 3 of CN4 negative so that the tray motor rotates in the direction in which the tray is closed. Conversely, the signal at "L" is also inversion-amplified in IC3 (1/2) to turn ON Q15 so that the tray motor rotates in the direction in which the tray motor rotates in the direction in which the tray motor rotates in the direction in which the tray motor rotates in the direction in which the tray motor rotates in the direction in which the tray motor rotates in the direction in which the tray motor rotates in the direction in which the tray is opened.
In addition, when pin 9 of IC15 is opened, pin 2 of IC3 is at zero voltage so that the tray motor stops since no voltage is applied.
(This circuit is effective only at kick operation.)
Both IC12 (2/2) and IC13 (1/2) output "H" signals in normal operation. Thereupon, when the tracking error voltage at pin TE output goes up more than about +0.6 V, pin 2 of IC12 (2/2) becomes "L" and this voltage is applied to TEG 1 input of IC15. See "1" in the table below.
State | TE Voltage | TEG1 | TEG2 | ||
---|---|---|---|---|---|
1 | >+0.6 | L | Н | ||
2 | <-0.6 | Н | L |
Table-1 | |
---|---|
I UDIC I |
Conversely, when the tracking error voltage at TE output goes down less than -0.6 V, pin 2 of IC12 (2/2) becomes "H" and pin 2 of IC13 (1/2) "L" so that this voltage is applied to TEG 2 input of IC15. See "2" in the table above. The search time is shortened by this control circuit. Normally, in play mode, this voltage is offset by signal TEP, therefore inputs TEG 1 and TEG 2 are invalid.
The peak hold circuit consists of Q23 to Q26, D28 to D35, IC14 (1/2), etc. When KGC becomes "H" on kick state, Q23 and Q24 turn ON, and Q25 and Q26 turn OFF. Thereby, C70 is charged with the positive peak voltage at tracking error input TE and C69 is charged with the negative peak voltage. During kick, C69 and C70 are continuously charged with these peak voltages. When the unit returns to normal play from the kick state, Q23 and Q24 turn OFF and Q25 and Q26 turn ON. Then, the average value of the voltages at C70 and C69 is input to IC14 (1/2). Here, it is subject to subtraction with the value of voltage TE, so that the unit is restored to normal play from the kick state.
This noise limiter consists of IC14 (2/2) and Q27 to Q30. Q29 is the limiter ON/OFF switch. When signal TEP is "L" (during kick), no limiter operation is possible. Normally, Q29 is OFF during play.
The tracking error (TE) voltage is amplified to about 6 times in IC14 (2/2) and is applied to the bases of Q27 and Q28 through an HPF consisting of C73 and others. When the voltage goes up more than about +0.6 V, Q27 turns ON, while when it goes down less than about -0.6 V, Q28 turns ON. During that ON period, the peak noise of the voltage is suppressed so that the following stage gets free from the disturbance caused by this noise. Thereby, the pickup is prevented from jumping off the correct track to another one due to noise.
Signal RFES produced in IC10 (2/2) becomes "H" when the RF signal level is discreased by flaws or dust on the disc. This signal at "L" is output as signal DIN from the dropout control block in IC15 to the disc flaw position memory circuit in which positional data of flaw is stored. At the same time, this signal is also output as signal DCON which is the tracking servo gain reduction gate pulse. Dropout control is thus made. Pin DIN of IC15 outputs a signal indicating the RFES state at the rising edge of signal DOCK. It also checks the output of the disc flaw position memory circuit (pin 8 of IC7) at the falling edge of signal DOCK and then outputs signal DCON (pin 12 of IC15) to tracking servo amp circuit.
For play, the actuator of the pickup is moved up or down by the 2 Hz signal from F.SRCH (pin 2 of CN2). At this time, when the disc is in rotation, the BE signal is output from the pickup only at the moment the laser beam is focused. With the RF signal. IC10 (1/2) outputs an "L" signal (RFOK) to turn ON Q31. Further, this signal is inverted at IC16 and FOK becomes - 12 V. Q2 and Q6 is turned off by "L" FOK signal, "H" LDC signal is inverted to "L" to turn Q4 off, so that the focus servo starts operation. Thus, a continuous RF signal appears at pins 6 and 7 of CN6 from the pickup. Thereby, pin 14 (FOKG) of IC15 outputs an ''H'' signal. This signal is inverted at IC16. The voltage at pin 11 of IC15 becomes - 12 V. Therefore, Q12 turns OFF so that IC2 (2/2) can perform amplification. In addition, DCON is "L" as long as the level of the RF signal does not drop suddenly due to flaws or dirt on the disc. As the KGC line is at -12 V in normal play (except for the kick state), Q7, Q8, Q9 and Q12 are all OFF. Thus, the tracking servo works so that the pickup traces the pit sequence on the disc. The data on the disc can thereby be read out continuously.
The EFM signal (EFMO) output from pin 41 of IC15 on the servo PCB is input to pin 52 (EFM 2) of IC8 and pin 14 (EFMI) of IC9 on the process PCB.
IC9 works as a digital PLL together with VCO Q3. Signal EFMI is phase-compared with signal PLCK (4.32 MHz) resultant from 1/4 frequency division of signal VCOI.
Here, when signal PLCK is delayed from signal EFMI, pin Uovr becomes "L" and acts to make the VCO frequency higher. Conversely, when it is advanced, pin Dovr becomes "H" and acts to make the VCO frequency lower.
The EFM signal output from pin Dovr in synchronization with the rising edge of signal PLCK is fed to pin 53 (EFMI) of IC8, in which detection is made to a frame sync signal which is a continuous signal of 11 "H" bits and 11 "L" bits.
When the frame sync signal is obtained, the EFM signal is demodulated into an 8-bit signal. Moreover, the user's bits just after the frame sync signal are demodulated and data Q among them are displayed as time data bundled by 98 frames. These are also used in FF or BWD operation, etc.
The music data, converted from 14-bit to 8-bit signals, are written in jitter absorption memory IC7 under control of IC6 (TC9179F). The one-frame 32-symbol data is corrected for error in the C1 correction section. Next, after de-interleave operation, the data which could not be corrected in the C1 correction section is corrected in the C2 correction section.
Only the data which could not be corrected even in the C2 correction section is subject to mean-value interpolation and is output to the D/A converter.
The signal resultant from 1/4 frequency division of frame sync signal and the input signal (2.1168 MHz) from C21K are used here. Then, with the center of the count of 1152 clock pulses of C21K in respect to the former signal, pin 20 (AFCO) outputs a 0 V signal when the speed of the disc motor rises about 10% and outputs a 5 V signal with the same voltage as voltage VDD when the speed lowers about 10%. Thus, in the range of ± 10% change in motor speed, the output voltage corresponds to motor revolution (PWM wave).
Phase-comparison is made between the signal resultant from 1/8 frequency division of the frame sync signal and the signal from a frequency division of signal C21K. The comparison output is emitted as PWM signal with 8-bit resolution. Here, VDD/2 (2.5 V) is output at a phase difference of zero in a control range of ±7/8 π.
In addition, the speed of the disc motor can be controlled by signal DIV + or DIV- from TC9179F. For information about TC9178F and TC9179F, refer to the diagram on pages 81 to 90.
The serial music data, which is output from IC6 on the process PCB, is input to the D/A converter (IC21) at the falling edge of signal BCK. The data of one word is transferred to IC21 by repeat input at 16 cycles of signal BCK. After that, when signal CC drops down to "L", a pulse (DCR or DCL) is output with which the integrator output is discharged. Then, after clearing the previous sampled value, signal IOUTR or IOUTL is continuously output according to the level of signal LRCK during the time in proportion to the amount of the digital music data and is held as an analog voltage at integration capacitor C212 or C213. The example of waveform ① in Fig. 1-4A represents a sequence of this state. ② Fig. 1-4A shows the waveform when signal IOUTR or IOUTL is sampled by signal LRCK. When this PAM wave is filtered by an LPF,
this LPF outputs a music signal with a peak amplitude of 1/2 that of the PAM wave. This music signal is input to buffer amplifier IC27 to which a frequency characteristic compensotor CR circuit is connected.
IC26 controls the emphasized signal detected by IC8. Pin EMPH of IC8 outputs an "H" signal with a disc on which emphasized signals are recorded, and thus the de-emphasis circuit works. The muting relay connected to the output pin is controlled by the muting signal from the micro-processor. In addition, IC21 judges the music data as an R-ch signal while signal LRCK is "L". During this period, IC6 outputs L-ch signals. Therefore, signal IOUTR of IC21 is handled as an L-ch signal and signal IOUTL as an R-ch signal.
Fig. 1-4A D/A Converter Circuit
Fig. 1-5-1-1
VÐD (4) (I5)Res
Fig. 1-5-1-2 Timing Chart for IC13 Reset Signal
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1-5-2 TRAY OPERATION
TRAY | OP | ENS | CLC | SES | Remarks |
---|---|---|---|---|---|
Mode | E | F | 8 | с |
Refer to control MODE of
IC15 (TC15G008AP) Table 2-2B and notes below. |
1 | L | н | L | L | |
2 | н | н | L | L | |
3 | н | н | L | н | |
4 | н | н | н | н | |
5 | 1. | L | L | E. |
P-11NNR/TI NP-11NNR/TI
1. CIRCUIT DESCRIPTION
Fig. 1-5-3-2 Timing diagram for LASER ON TIME
When a signal to activate the laser is applied to pin 24 to 27 of IC15 (TC15G or T7001) from the system control microprocessor, the level at pin 11 changes from "L" to "H" and the level at pin 3 of IC16 also switches from "L"
1-5-3 LASER ON OPERATION
1-5-4 FOCUS SEARCH OPERATION
When a disc is set and the tray is closed , a signal of 2 Hz is output maximum four times to pin 36 of microprocessor IC15 (TMP4740N). This signal confirms that the disc has been properly set and prepares for focus servo operation. The focus servo maintains a constant position of the pick-up lens against the disc so that the size of the focused laser spot is kept constant as a result. If the distance between the pickup and the disc is to far or too close, a proper size of the laser spot can not be obtained on the disc surface, in another words, not properly focused.
Fig. 1-5-4-2 Operation Timing of Focus Search
1-5-5 DISC DETECTION OPERATION & REVERSE-REVOLUTION PREVENTION CIRCUIT FOR DISC MOTOR
3. The HFOK signal is to judge the presense of RF signal as explained above. It results in "L" when the RF signal is present and it results in "H" when not present. Both of the MSP and RFOK signals are "H", when the disc motor starts running (initial start from a complete stop state.) Q31 and Q19 go to QFF, while Q18 is QN. This increases a negative voltage at pin 8 of IC4 (1/2), horeby preventing the disc motor from revolving in the reverse direction.
1-5-6 FG & DISC MOTOR DRIVE AND STOP OPERATIONS
44
1-5-7 FOCUS SERVO OPERATION
1-5-8 TRACKING SERVO OPERATION
7. The output available at pin 8 of IC2(2/2) is applied
DP-1100B/TI DP-1100B/TI
1-5-10. SEARCH AND LOCK-IN CIRCUIT OPERATION DURING KICK MODE
Pin 23 (RFG) of IC15 (TC15G or T7001) is at "L" level during the kick mode. The RFG signal is fed to pin 1 of IC18 and the inverted output of the level-shifted RFG signal (named KGC) is output to pin 15. It is "H" level dur-ing the kick mode, The signal is applied to the base of O2 through R33, turning Q7 ON under the kick mode to cut the tracking servo loop. The tracking error signal (pin 8 of IC12 (1/2) during the kick mode is a sawtooth waveform as shown, but the contror fits amplitude is not always in line with D V (some offset results). This may possibly cause unstableness, when the unit changes to a normal FLAY mode from the kick mode (when the tracking servo i SON). To solve this problem, the KGC signal (+5 V during kick mode and -12V during FLAY mode) is given to the heses of Q23 and Q26 are OFF during the kick mode.
The diodos D29 and D31 and G3 and threshold as below: 1.5 V + 0.6 V (D29) - 0.6 V (D31) = 1.5 V The 1.5 V is charged across C70.
Part (B) The -0.5 V is charged across C69.
PLAY
When the unit is switched from KICK to PLAY, Q26 and Q25 turn ON, C69 -0.5 V+C70+1.5 V=1.0 V is ap-plied to pin 6 of IC14 (1/2) and the output from pin 8
49
1-5-11. PU DRIVE OPERATION
Fig. 1-5-11
Since control of the pickup feed motor should gradually be made just to componsate an offset of the tracking error signa during a normal PLAY mode, it is done by TCO+tracking coll+1 signal only. During a normal PLAY mode, the TCO+signal is applied to pin 7 of IC3 (22) through R74 Since PLAY is -12 V (pulled-down output of IC16) during normal PLAY mode, 014 is OFF. In this state, IC3 (22) and RC components form a low-pass filter. As a result, the high frequency components are eliminated from TCO+ signal to obtain offset signal. It is applied to pin 3 of IC4 (2/2) through R78. After gain adjusted, it drives the pickup carry motor through R80 and L3.
1-5-12. FOCUS SERVO CONTROL SIGNAL OPERAITON
tion is discontinued when the laser diode is not being ac-tivated. 5. A "H" level output is applied to pin 1 (TEP) of IC15 only during normal PLAY mode. It, however, becomes "L" level, when a kick signal is given during the normal PLAY mode. The signal is integrated by R210, R209, D36 and C74 to turn on Q29 and Q30. In this instance, Q27 and Q28 are placed under OFC condition by making Q30 turn Q18 are placed under OFC condition by making Q30 turn Q14 during the kick mode. The noise limiter circuit is thus disabled during search mode.
NP-11008/11 NP-11008/11 1. CIRCUIT DESCRIPTION
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1-5-14. SERVO CONTROL CIRCUIT OPERAITON
8. For example, when the microprocessor indicates (INH, A, B C)= (L, L, pin 13 of 0102 is connected to pin 3 of 0102. Thus, 24 kB resistance is connected in parallel with the 15 kB resistance already inserted between pins 1
Q102
pin No. |
Q102 input
INH |
Q102 input
A |
Q102 input
B |
Q102 input
C |
ut PU alignment
level Resistance |
Resistance value between
pins 1 and 2 of Q103 |
|
---|---|---|---|---|---|---|---|
6 | н | L | L | L | INH | 80 | 15 k |
12 | L | н | н | L | . 3 | 180 k | 13.8 k |
1 | L | L | L. | н | 4 | 82 k | 12.7 k |
5 | L | н | £. | н | 5 | 51 k | 11.6 k |
2 | Ļ | L | н | н | 6 | 39 k | 10.8 k |
4 | L | Н | Н | н | 7 | 30 k | 10 k |
13 | L | L | L | L | 0 | 24 k | 9.23 k |
14 | L | н | L | L | 1 | 20 k | 8.57 k |
15 | L | L | н | L | 2 | 16 k | 7.74 k |
NP-1100R/II NP-1100R/II
Tracking error pulse control signal is present at pin 1 (TEP) of IC15 and it is "H" level during the normal PLAY mode. It, however, switches to "L" level during KICK mode. This is input to pin 3 and 12 of IC3 to disble the circuit during
54
Mode
Signal |
Normal | Long (More than |
Search
512 tracks) |
Short
(Less than |
Search
512 tracks) |
- | REV |
---|---|---|---|---|---|---|---|
PLAY |
FF
Direction |
REV
Direction |
FF
Direction |
REV
Direction |
FF | ||
KICF | 2.5V | 2.5 | 2.5 | ||||
PUFF | 2.5V | 5 | 0 | 2.5 | 2.5 | 2.5 | 2.5 |
i
Intel Clanel durin |
a cook Mada |
i
Applies reverse |
Linds (N/) |
Applies reverse to put a brake.
1-5-16. KEY DATA AND TIMING PULSE OPERATION
Since the unit has many function keys, a 6 x 4 matrix had been made in order to make the best use of the input/out-put ports of IC1 (4-bit microprocessor). The key input can be judged by key scanning pulses from IC1 (6 lines in time division) and four key input lines.
2. Pin 11 to 16 of IC1 are periodically providing the pulses staggered by a regular timing as shown. Each of them enters the vertical line of the key matrix through a diode, which prevents more than 2 keys from being pressed at the same time. The 26 to 29 are input lines and they are alf 0 V when no keys are pressed. The pin 14 line and pin 26 are shorted, and scanning pulse from pin 14 is input to pin 26. IC1 (4-bit microprocessor) recognizes that the PLAY key is pressed. The pin 14 line and pin 26 are shorted, and scanning pulse from pin 14 is input to pin 26. IC1 (4-bit microprocessor) recognizes that the PLAY key has been pressed, based on the input to pin 26 and the timing of pulse at pin 14 and gives the PLAY instruction to IC16 (control microprocessor). The reason that the timing pulse has a double frequency at pin 16 is that two clock signals are entered simultaneously, when M-READ and CLEAR keys are pressed at same time.
Fig. 1-5-16-2 IC1 Timing Pulse Waveform
55
-0 *
3. R21 and R22 are resistors to detarmine a reference voltage for the filter, and INA + is usually held at about 2.7 V. During the SEARCH mode, however, the reference voltage is raised up (about 3 V) to shorten the search period. For this purpose, an RFG signal of "L" level is applied to the base of 015 to Linn (IOA and is "H" outputs a dded to INA + through R110 during the SEARCH period. A The output from pin 4 (OUTA) of low-pass filter output controls voltage for VC0 through R15. The VC0 has been designed to coslite at e about 16 MHz to 19 MHz with a control voltage arange of 1 V to 8 V. Under normal PLAY condition, it is osalilating at about 17 MHz with a control voltage at a maximum of 8 V and D5 is a vanable capacitance dide. If Grave a blas to Q3 and D33 is a term redice Tig.
5. An oscillation amplitude of VCO is about 500 mVp-p. Eliminating the DC component by C19, it is applied to pin 9 of IC9. Being amplified in IC9 and 1/4 frequency divided, the output is available at pin 12.a s ELCK. (The PLCK is about 4.3 kHz during normal PLAY mode) EFMI input to pin 14 is synchronized by the PLCK, and the DOUT output is available at pin 13. 014 and 013 are connected in an emitter follower configuration and work as a buffer for the PLCK and DOUT signals are observed with the PLL circuit at the normal PLAY condition, the clean waveform is locked as shown in the diagram at right.
1-5-19. MUTING CIRCUIT OPERATION
3. When bad conditions of a disc (scratches or dust) make the adequate correction and compensation impossible because of too many errors in the EFM signal even during normal PLAY mode, pin 35 and 36 become "L" level. Pin 34 of IC6 turns to "L" level by a wired OR connection. The digital muting is thus accomplished by turning the 16-bit digital signal OFF.
1-5-20. REMOTE CIRCUIT OPERATION (TRANSMITTER HAS A SIMILAR OPERATION AS TV OR VIDEO AND WILL NOT BE EXPLAINED)
A data signal (modulated by a 38 kHz carrier) sent from the transmitter enters to infrared ray sensor diode PH1. PH1 varies the current through it by changing its internal resistance in accordance with the input signal. The quies-cent point current is determined by load resistor R29 and +B supply. The varying current signal is fed to pin 7 of remoto contol amp (C17. It is about 40 dB amplified here and the output is available at pin 1. The signal is fed again to pin 2 of IC16 through the detec-tion circuit of D14, amplification centering around 38 kHz. The output appears at pin 7. The signal wave/orm-shaped by IC16 as shown at right is fed to pin 37 of IC1 for the control purpose of the microprocessor.
Fig. 1-5-20
59
1-5-21. EMPHASIS CIRCUIT OPERATION
Fig. 1-5-21-2 Frequency response of high-end cut
Q103 (TA7731P) is the head amp and operation IC for the laser beam receiver device, developed for CD system DAD player.
Fig. 2-1A
Block diagram
Fig. 2-1B
NR/
Pin functions
Pin No. | Symbol | Description | Remarks |
---|---|---|---|
1 | OUT1 |
Pin which outputs the sum signal (A + B) of pin IN A and IN B input signals out of 4-division photodetector outputs.
The final stage buffer amp is provided with an external feedback resistance to neutralize the effect of the irregularity in characteristics between photodiodes. |
FC I
RF1 OUT I Buffer amp Note 1 With max. input of 100 kHz Transfer impedance |
2 | FC1 |
Final stage buffer amp negative input pin of OUT1 output signal.
A resistance is connected between this pin and pin OUT1 to control the gain. |
= 27 κα
R F1 = 9 kΩ (typical) |
3 | GND2 | GND pin | |
4 | IN A | Input pin of signal A (one of 4-division photodetector outputs) | Note 1 |
5 | IN B | Input pin of signal B (one of 4-division photodetector outputs) | |
6 | IN C | Input pin of signal C (one of 4-division photodetector outputs) | |
7 | IN D | Input pin of signal D (one of 4-division photodetector outputs) | |
8 | GND1 | GND pin | |
9-10 | NC | Not connected | |
11 | V cc | Positive supply voltage pin | |
12 | OUT4 | Pin which outputs the sum signal (B + D) of pin IN B and IN D input signals out of 4-division photodetector outputs. | |
13 | OUT3 | Pin which outputs the sum signal (A + C) of pin IN A and IN C input signals out of 4-division, photodetector outputs. |
Note 1
With max. input of 100 kHz Transfer impedance = 27 kΩ (typical) |
14 | Vee | Negative supply voltage pin | |
15 | FC2 |
Final stage buffer amp negative input pin of OUT2 output signal.
A resistance (for feedback) is connected between this pin and pin OUT2 to control the gain. |
Pin No. S | Symbol | Description | Remarks |
---|---|---|---|
16 OU | JT2 |
Pin which outputs the sum signal (C + D) of pin IN C and IN D input signals out of 4-division photodetector outputs.
The final stage buffer amp is provided with an external feedback resistance to neutralize the effect of the irregularity in characteristics between photodiodes. |
FC2
FC2 BF2 OUT 2 m Buffer amp Note 1 With max. input of 100 kHz Transfer impedance = 27 kΩ R F1 = 9kΩ |
Table 2-1A
TC4051BP, of 8-channel configuration, is a multiplexer capable of selecting analog or digital signal, or combining them. The switch pin corresponding to each channel turns ON with the digital signal from the control pin.
JTS | "ON" CHANNEL | |||
---|---|---|---|---|
INHIBIT | С | в | A | TC4051BP |
L | L | L | L | 0 |
L | Ĺ | L | Н | 1 |
L | L | н | L | 2 |
L | L | н | н | 3 |
L | H | L | L | 4 |
L | н | L | н | 5 |
L | н | н | L | 6 |
L | н | н | Н | 7 |
Table 2-1C
2-2-1 IC9 (TC5050P) dropout memory, 50-stage/114-stage selection type shift register
3 4 2 DIN2 DOUT 5 1 DIN1 CLOCK NC ; 7, 15 12 6 11 VDD ; 16 VDD ; 16 VSS ; 8 13 DIN2 DOUT 10
Truth table
Block diagram
t", t"+1 | t, | +50 | t n+64 | ||||
---|---|---|---|---|---|---|---|
D IN1 | D IN2 | IM | ОМ | Dour | ОМ | Dour | |
Н | * | н | L | н | н | н | |
L | * | н | L | L | н | L | |
* | Н | L | L | Н | н | н | |
* | L | L | L | L | н | L |
2-2-2 IC15 (TC15G008AP) semi-custom IC
Pin connection
■ ; I/O port
Fig. 2-2-2A
Block diagram
Fig. 2-2-2B Internal block diagram
Pin functions
Pin No. | Symbol | Pin name | IN/OUT | Remarks | |||||||
---|---|---|---|---|---|---|---|---|---|---|---|
1 | TEP |
Tracking error pulse con-
trol output |
0 |
Out
the |
puts a ''H
kick signa |
ʻʻ signal o
al is outpu |
nly during play. However, it becomes ''L'' wh
t during play. |
ien | |||
TEG1 | TEG2 | Function | |||||||||
2 | TEG2 |
Tracking error detector
control (1) input |
1 | Н | Н |
Tracking error detection and normal oper-
ation |
Pullup resistor
incorporated |
||||
L | Н |
TEOP outputs a ''H'' signal at the timing
of the absolute phase difference between TS1 and TS2. TEON is fixed to ''H''. |
|||||||||
Η | L |
TEON outputs a ''L'' signal at the timing
of the absolute phase difference between TS1 and TS2. TEOP is fixed to ''L''. |
|||||||||
6 | TEG1 |
Tracking error detector
control (2) input |
L | L |
Stop of tracking error detection. TEOP is fixed to "L".
TEON is fixed to "H". |
||||||
3 | TEON |
Tracking error negative
output |
0 |
Whe
(at n |
When TS2 advances in edge phase against TS1, outputs a "L" signal (at normal operation). | ||||||
4 | TEOP |
Tracking error positive
output |
0 | Whe |
en TS2 de
nal operat |
lays in edç
ion). |
ge phase against TS1, outputs a ''H'' signal ( | at | |||
5 | TES |
Tracking error polarity in-
dication input |
I | Cont | trol signal | input use | d in kick control for search operation |
Pullup resistor
incorporated |
|||
7 | TTAC | Track TAC output | 0 |
Pin o
pletio |
outputs cloon of kick |
ock pulse
or the co |
which the microprocessor is informed of cor
unt number of tracks. |
n- | |||
8 | PUD | PU motor control input | l |
Inpu
carry |
it which s
γ signal is |
tops the P
a specific |
U motor only when the PU motor compulsor
code (PUD = ''H''). |
·γ- | |||
9 | OPNS | Open/close output | 0 |
Outŗ
''L'' |
out for dis
= open, |
3-state output | |||||
10 | DSG | Data slice control input | 1 |
Inpu
circu ''H'' |
it for cont
uit. ' input = |
trol signal
OFF. |
which stops the sub-control of the data sli | се |
Pullup resistor
incorporated |
Pin No. | Symbol | Pin name | IN/OUT | Description | Remarks |
---|---|---|---|---|---|
11 | LDC |
Laser diode control out-
put |
0 | Laser diode ON = ''H'' output, OFF = ''L'' output | |
12 | DCON | Dropout control output | 0 | Output which indicates the dropout position of the RF signal. | · |
13 | PLAY | Play control output | 0 | Control signal output which operates the PU motor by the PU tracking servo signal. | |
14 | FOKG | Focus OK output | 0 |
Outputs the OK signal on instruction from the microprocessor when the laser spot is focused.
Focus ON = "H" output. |
|
15 | MSP | Disc motor control output | 0 | Output for disc motor ON/OFF control signal. | |
16 | TPCO | TES polarity select input | I |
Input for signal which selects the polarity of the TES signal used in the kick process circuit.
Open (V pp ) or connected to GND. |
Pullup resistor
incorporated |
17 | EFMI | EFM signal input | l |
Input for binary signal obtained by passing the RF signal regenerated by the PU through a comparator.
Its polarity should be positive against the RF signal polarity. |
Pullup resistor
incorporated |
18 | TS2 |
Tracking error generation
signal (1) input |
I | Input for binary signal obtained from passing the A 2 + A 4 signal of 4-division photodetector through zero-cross comparator. (Used in tracking error generation.) |
Pullup resistor
incorporated |
19 | TS1 |
Tracking error generation
signal (2) input |
ļ | Input for binary signal obtained from passing the A 1 + A 3 signal of 4-division photodetector through zero-cross comparator. (Used in tracking error generation.) |
Pullup resistor
incorporated |
20 | RFOK | RF signal OK input | I | Input for signal indicating the regeneration of the RF signal by the pickup. It turns OFF the data slice (sub) and output EFMO. (At "H") |
Pullup resistor
incorporated |
21 | GND | GND | |||
22 | RFES | RF envelope signal input | I |
Input for RF presence/absence signal, this signal is obtained by passing
the RF envelope detection signal through comparator. It is used in the kick process and dropout process sections. |
Pullup resistor
incorporated |
Pin No. | Symbol | Pin name | IN/OUT | Description | Remarks |
---|---|---|---|---|---|
23 | RFG |
RFES control signal out-
put |
Ο |
Output which controls the detection level of signal RFES. "L" only dur-
ing kick operation. |
|
24~27 |
MODE4~
MODE1 |
Mode select signal input | I |
Input for servo system control signal generation and kick operation pro-
cess direction indication. Connected to the microprocessor. |
Pullup resistor
incorporated |
28 | DSL1 |
Data slice control (1) out-
put |
О |
Output for signal obtained by passing signal EFMI through the internal
buffer amp. Has the same polarity as signal EFMI. |
|
29 | DSL2 |
Data slice control (2) out-
put |
Ο |
Output for data slice control sub circuit.
Detects the variation in slice level by check of the jitter of signal EFMI to control the slice level at an optimum level. |
|
30 | MODE-0 | Mode select signal input | I |
Input for servo system control signal generation and kick operation pro-
cess direction indication. Connected to the microprocessor. |
Pullup resistor
incorporated |
31 | TEST | Test | ł | Normally, open or connected to V pp . |
Pullup resistor
incorporated |
32 | PUFF |
PU motor fast-carry signal
output |
0 | ''H'' output → FWD, ''L'' output → BWD, HiZ → OFF | 3-state output |
33 | KICF | PU kick pulse output | о | ''H'' output → FWD, ''L'' output → BWD, HiZ → Kick OFF | |
34 | DIN | Dropout data I/O | 1/0 | Data I/O connected to shift register for dropout control | |
35 | DOCK |
Dropout control clock
pulse output |
0 | Output for clock signal (with 6 times the FGS frequency) connected to shift register for dropout control | |
36 | FG4 | FG signal output | о | Output for clock signal obtained from 30 division of signal DOCK | |
37 | CK88 | 88 kHz clock pulse input | Input for approx. 88 kHz reference clock signal |
Pullup resistor
incorporated |
|
38 | MUT | Muting output | 0 | Output for muting audio signal. |
Pullup resistor
incorporated |
Pin No. | Symbol | Pin name | IN/OUT | Description | Remarks |
---|---|---|---|---|---|
39 | FGS | FG signal input | I |
Input for FG signal with 20 pulse/disc rotation.
Should have a duty ratio of approx. 50. |
Pullup resistor
incorporated |
40 | PLCK | PLL section clock pulse input | I | Input for reference signal (4.32 MHz) to PLL section for EFM signal reading |
Pullup resistor
incorporated |
41 | EFMO | EFM output | О |
Inversion output of signal EFMI.
With signal RFOK ''H'', is fixed to ''L''. |
|
42 | ۷۵۵ | V DD | +5 V |
Table 2-2A
Each data for mode 0 to 3 is passed through the latch circuit, thereby different control signals are generated in the decoder section.
Control mode truth table A)
MODE | *5 | *7 | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
0 | 1 | 2 | 3 | 4 | TEP | PLAY | FOKG | LDC | MSP | MUTE | PUFF | OPNS | STATE | |
0 | 0 | 0 | 0 | 0 | ο | 0 | 0 | 0 | 0 | 0 | 0 | HiZ | HiZ |
|
1 | 0 | 0 | 0 | 0 | 1 | 0 | 0 | 0 | 1 | 0 | 0 | HiZ | HiZ | At judgement of disc's loading. |
0 | 1 | 0 | 0 | 0 | 2 | (1) | 1 | 1 | 1 | 1 | 1 | HiZ | HiZ | 1 REV 2 Cue 3 Play mode (1) x 2 |
1 | 1 | 0 | 0 | 0 | 3 | (1) | 1 | 1 | 1 | 1 | 0 | HiZ | HiZ |
BWD kick, REV, F REV, FWD kick, FWD, F FWD,
Judgement of right/reverse side of the disc, TOC read. |
0 | 0 | 1 | 0 | 0 | 4 | 0 | О | 0 | 1 | 1 | 0 | HiZ | HiZ | Focus servo ON |
1 | 0 | 1 | 0 | 0 | 5 | 0 | о | 1 | 1 | 1 | 0 | HiZ | HiZ |
Pause mode (2) *3
Focus tracking servo ON |
0 | 1 | 1 | 0 | 0 | 6 | 0 | 0 | 1 | 1 | 1 | 0 | 1 | HiZ | FWD search |
1 | 1 | 1 | 0 | 0 | 7 | 0 | 0 | 1 | 1 | 1 | 0 | 0 | HiZ |
BWD search,
Stop-BWD mode |
0 | 0 | 0 | 1 | 0 | 8 | 0 | 0 | 0 | 1 | 0 | 0 | HiZ | 1 |
Tray
close (laser diode: ON) |
1. | 0 | 0 | 1 | 0 | 9 | (1) | 1 | 1 | 1 | 1 | 0 | 0 | HiZ | PU motor kick before BWD search |
0 | 1 | 0 | 1 | 0 | А | (1) | 1 | 1 | 1 | 1 | 1 | (1) *6 | HiZ | Play mode (2) *4 |
1 | 1 | 0 | 1 | 0 | в | (1) | 1 | 1 | 1 | 1 | 0 | 1 | HiZ | PU motor kick in FWD search |
0 | 0 | 1 | 1 | 0 | С | 0 | 0 | 0 | 0 | 0 | 0 | HiZ | 1 | Tray close (laser diode: OFF) |
1 | 0 | 1 | 1 | 0 | D | 0 | 0 | 0 | 0 | 0 | 0 | 0 | HiZ | Eject-BWD mode |
0 | 1 | 1 | 1 | 0 | E | 0 | 0 | ο | 0 | 0 | 0 | HiZ | 0 | Tray open (Open from ON of PU, SLT SW) |
1 | 1 | 1 | 1 | 0 | F | 0 | О | о | 0 | 0 | 0 | 0 | О | Tray open (Open from OFF of PU, SLT SW) |
*1 Pause mode 1 The
The mot *2 Play mode 1 Norr *3 Pause mode 2 All ş *4 Play mode 2 Moc *5 TEP Moc case *6 PUFF Witt |
e beginn
en, 10 s tor) OFI rmal pla pause r de in w de whic se, a ''1 th code |
hing of t
sec later, F. ay mode modes o hich FW ch is eng '' outpu A, OUT |
he first t
pause r ther that /D pulse aged on it is emit |
une is n
node is n pause is outp ly a Lat ted. ts a ''1 |
neglecte
engage mode out perio ch-SP = '' outpu |
d, and t
d with L dically in 1 (sect t only a |
he unit
D and N n play n ion 5-1; t PUD = |
pauses.
1D (disc node 1 ). In this = 0. |
5 |
emitted in any mode.
Table 2-2B TC15G008AP Normal mode table
Search control used in music scan, etc. is performed by the kick control circuit.
MOD | )E | Stator | |||
---|---|---|---|---|---|
0 | 1 | 2 | 3 | (X) | 514101 |
0 | 0 | 0 | 0 | 0 | Kick Reset |
1 | 0 | 0 | 0 | 1 | Kick Reset |
0 | 1 | 0 | 0 | 2 | BWD1 TRACK KICK |
1 | 1 | 0 | 0 | 3 | FWD1 TRACK KICK |
0 | 0 | 1 | 0 | 4 | BWD3 TRACK KICK |
1 | 0 | 1 | 0 | 5 | FWD3 TRACK KICK |
0 | 1 | 1 | 0 | 6 | BWD5 TRACK KICK |
1 | 1 | 1 | 0 | 7 | FWD5 TRACK KICK |
0 | 0 | 0 | 1 | 8 | BWD7 TRACK KICK |
1 | 0 | 0 | 1 | 9 | FWD7 TRACK KICK |
0 | 1 | 0 | 1 | А | BWD15 TRACK KICK |
1 | 1 | 0 | 1 | В | FWD15 TRACK KICK |
0 | 0 | 1 | 1 | С | BWD31 TRACK KICK |
1 | 0 | 1 | 1 | D | FWD31 TRACK KICK |
0 | 1 | 1 | 1 | E | BWD CONTINUOUS Kick |
1 | 1 | 0 | 0 | F | FWD CONTINUOUS Kick |
Table 2-2C TC15G008AP Kick mode table
2-3-1 IC15 (TMP4740N-5909, 5914) Main microprocessor
Pin No. | . Port name |
Signal
name |
IN/OUT | Level | Function/operation | |
---|---|---|---|---|---|---|
1 | R40 | MD0 | 0 | L | Outputs various mode data and kick data outputs to IC15 (TC15G008AP) for interface with the servo system. | |
2 | ku | R41 | MD1 | 0 | L | Outputs various mode data and kick data outputs to IC15 (TC15G008AP) for interface with the servo system. |
3 | R4 | R42 | MD2 | 0 | L | Outputs various mode data and kick data outputs to IC15 (TC15G008AP) for interface with the servo system. |
4 | R43 | MD3 | 0 | L | Outputs various mode data and kick data outputs to IC15 (TC15G008AP) for interface with the servo system. | |
5 | R50 | MD4 | ο | L | Data select signal output to IC15 (TC15G008AP). (The kick control data at "H" level and the mode control data at "L" level.) | |
6 | RE | R51 | SVCS | I/N | L | Operation start/stop control signal to the servo control microprocessor IC12 (MB88201) |
7 | no | R52 | A2 | 0 | L | Address data output to the external RAM IC14 (TC-5514P). |
8 | R53 | A1 | 0 | L | Address data output to the external RAM IC14 (TC-5514P). | |
9 | R60 | AO | 0 | Н | Address data output to the external RAM IC14 (TC-5514P). | |
10 | R6 | R61 | A3 | 0 | Н | Address data output to the external RAM IC14 (TC-5514P). |
11 | 110 | R62 | Α4 | 0 | н | Address data output to the external RAM IC14 (TC-5514P). |
12 | R63 | A5 | 0 | Н | Address data output to the external RAM IC14 (TC-5514P) | |
13 | R70 | D0/QDAd | 1/0 | Н |
|
|
14 | D7 | R71 | D1/QDAC | I/O | н |
|
15 | 17 | R72 | D2/QDAb | I/O | Н |
|
16 | R73 | D3/QDAa | I/O | н |
|
|
17 | P10 | A6 | 0 | н | Address data to the external RAM IC14 (TC5514). | |
18 | D1 | P11 | A7 | о | Н | Address data to the external RAM IC14 (TC5514). |
19 | с I | P12 | A8 | 0 | Н | Address data to the external RAM IC14 (TC5514). |
20 | P13 | A9 | о | н | Address data to the external RAM IC14 (TC5514). |
Table 2-3-1A
Pin No. | Port | ort name Signal name | IN/OUT | Level | Function/operation | |
---|---|---|---|---|---|---|
22 | P20 | R/W | о | Н | Read/write control signal to the external RAM IC14 (TC5514). (''H'' level in read mode and ''L'' level in write mode) | |
23 | 00 | P21 | QDSE | 0 | Н | Data input select signal to R7 port. (Data from the external RAM IC14 (TC5514) at "H" level and the data input of the subcode Q from IC8 (TC-9178) at "L" level) |
24 | ٣2 | P22 | QDAS | 0 | ΨĽ | CRC error check data and subcode Q data select signal. (Error data at ''L'' level and Q-data at ''H'' level) |
25 | P23 | QDARD | 0 | Ĺ | A signal to read the subcode Q data from IC8 (TC-9178) in 4-bit units. (Data is updated at ''H'' level. One cycle ends every 19 times.) | |
26 | K00 | CLS/RFG | I | * |
|
|
27 | KO | K01 | Marana | ٠ |
|
|
28 | κυ | K02 | SLT | I | * | Pickup position detect signal input (''H'' level when the pickup is positioned in the program area and ''L'' level in the read-in area.) |
29 | K03 | RFOK | Ι | * | RF signal input (''L'' level when RF signal exists.) | |
35 | R80 | IRQ | 1/0 | Н |
Data transfer request signal from IC1 (TMP47C41N)
Usually ''H'' level and goes to ''L'' level when the request exists. |
|
36 | R81 | FSRH | О | L |
Focus search signal (≒2 Hz)
Usually ''L'' level. |
|
37 | R8 - | R82 | QDRE | l | Н | A signal to enable reading the subcode Ω data from IC8 (TC-9178). |
38 | R83 | TTAC | I | Н | Kick end signal | |
39 | R90 | DAT21 | 1/0 | L |
|
|
40 | R9 | R91 | DAT12 | 1/0 | Н | Serial data output to IC1 (TMP47C41N). |
41 | R92 | SCK | 1/0 | Н | Serial data transfer synchronizing signal | |
21 | V ss |
Power
supply |
Power supply (0 V) | |||
30 | TEST | ١· | Not used (Connected to V ss ) | |||
31 | - | ×w | I | _ | Oscillator connection terminal | |
32 | Xour | 0 | Oscillator connection terminal | |||
33 | RESET | I | Initialize signal input |
Pin No. | Port | Port name Sign | IN/OUT | Level | Function/operation | |
---|---|---|---|---|---|---|
34 | _ | V hh |
Power
supply |
Power supply (+5 V) | ||
42 | _ | V DD |
Power
supply |
Power supply (+5 V) |
Table 2-3-1A
IC9 (TD6315P), the PLL IC developed for CD system DAD player, consists of a digital phase comparator, a charge pump circuit, an active LPF and a data separation circuit.
The digital phase comparator detects the phase error between the clock pulse obtained from 4-division of the VCO output and the reference of the HF signal (EFMI) emitted from the data slicer. Then, from the charge pump circuit, up and down signals UO and DO are output as phase error data.
Pin connection diagram
Block diagram
Fig. 2-3-2B TD6315P Block diagram
Pin No. | Symbol | Description | Remarks |
---|---|---|---|
1 | INA+ |
Positive input of built-in OP amp.
Forms the guard ring of INA – together with pin 3 (NC) fixed to approx. 1/2 V ccp voltage. |
|
2 | INA – |
Negative input of built-in OP amp.
The signal subject to resistance addition by charge pump circuit outputs UO and DO and TC9178F pin TMO is input. |
|
3 | NC | Not used. This pin connected to pin INA + for giving isolation between pins INA – and OUTA. | |
4 | OUTA | Output of built-in OP amp. Connected to pin INA – through capacitor C and resistor R, forms a lag lead type filter to control VCO. | |
5 | V eea | Negative voltage supply to analog circuit. | |
6 | NC | Not used. Connected to pin INA + for giving isolation between pin V EEA and each of output pins UO and DO. | |
7 | υο |
Charge pump up signal output pin.
When signal PLCK obtained from 4-division of VCO frequency is phase delayed in rising edge against signal EFMI input, its "L" output duration is prolonged to make VCO fre- quency higher. In phase lock, "L" level = 1/2 PLCK. |
High impedance state ex-
cept during ''L'' direction. |
8 | DO | Charge pump down signal output pin. When signal PLCK obtained from 4-division of VCO frequency is phase advanced in rising edge against signal EFMI input, its "H" output duration is prolonged to make VCO frequency lower. In phase save, "H" level = 1/2 PLCK. |
High impedance state ex-
cept during ''H'' period |
9 | VCOI | Input pin of VCO output signal. The signal subject to AC coupling by a capacitor is input. | |
10 | GND | GND pin for digital circuit | |
11 | G |
Input by which charge pump outputs UO and DO are made into high impedance.
When made ''L'', high impedance mode is entered to hold the VCO frequency. |
TTL level |
12 | PLCK |
Output of data separation clock pulse generated from EFMI input signal in PLL circuit. This output, obtained from 4-division of VCO frequency (17.3 MHz), is input to PLCK of C-MOS processor TC9178F.
The clock pulse is 4.32 MHz with duty ratio of 50. |
C-MOS leve |
Pin No. | Symbol | Description | Remarks |
---|---|---|---|
13 | DOUT | Signal EFMI output. This output, synchronized with the rising edge of signal PLCK, is input to pin EFMI of C-MOS processor TC9178F. | C-MOS level |
14 | EFMI | Input for EFMI signal obtained by passing the RF signal regenerated from disc through data slicer. | TTL level |
15 | V ccp | Voltage supply to digital circuit. | |
16 | V CCA | Positive voltage supply pin to analog circuit. |
Table 2-3-2A
2-3-3 IC8 (TC9178F) E.F.M decoder Pin Description
Pin connection
Fig. 2-3-3A
1100R/11
TC9178F Block diagram
Fig. 2-3-3B
Pin No. | Symbol | 1/0 | Waveform | Description | Remarks |
---|---|---|---|---|---|
1 | NC | _ | Not connected | ||
2
3 |
PCSA
PCSB |
I |
These inputs determines the phase comparison frequency.
Phase comparison frequency = 7.35 kHz (frame sync signal)/N |
||
PCSA PCSB N fc (Hz) | |||||
L L 6 1225 | |||||
H L 8 918.75 | |||||
L H 17 612.5 | |||||
Н Н 16 459.375 | |||||
4 | DIV + | I |
5 V
0.5 µS 0 V (Appears only at low disc rotation.) |
Input for setting reference frequency division coefficient in APC signal generation circuit for CLV servo control.
Input as buffer memory status signal from TC9179F (IC6). In addition, the varying amount is selectable by DIVC. |
Connected to each of
TC9179F DIV+ (pin 65) and DIV- (pin 64) |
5 V
0.5 #S |
DIV + DIV - DIVC quency division coefficient Disc motor speed | ||||
5 | DIV | U ov | L L * 1/288 | ||
Ū | 2 | (Appears only at | H L L 1/287.5 Higher | ||
high disc rotation.) | H L H 1/287 Higher | ||||
L H L 1/288.5 Lower | |||||
L H H 1/289 Lower | |||||
6 | DIVC | 1 | Н Н 1/288 | ||
* Don't care | |||||
7 | C21K | 1 |
5 V
0.2 μS 0 V |
2.1168 MHz input. This signal, the clock pulse obtained from
4-division of X'tal OSC frequency 8.4672 MHz, is input from TC9179F (IC6). Its duty ratio is 50. |
Connected to CK2M
(pin 56) of TC9179F (IC6) |
8~10 |
TES-1 ~
TES-3 |
l | Test inputs, which operates normally at ''H'' or open state. |
Pullup resistor incor-
porated |
|
11 | NC | Not connected. | |||
12 | ЕМРН | 0 |
Output for emphasis presence/absence judgement represented by control bit of sub-code signal Q.
"'H'' = de-emphasis ON |
Table 2-3-3A
Pin No. | Symbol | 1/0 | Waveform | Desc | ription | Remarks | |||
---|---|---|---|---|---|---|---|---|---|
13 | 2/4S | 0 | _ |
Output for CH 2/CH 4 sele
of sub-code signal Q. "L" = CH 2, "H" = CH |
ection ju | dgement rej | presented by control b | oit | |
14 | FG IN | I |
5 V
10 mS 0 V (4 pulses/disc ro- tation) Near disc center Near disc edge |
Input for FG pulse from di
1 or 4 pulse per each rota the motor within the range Disc motor speed (rpm) -175 175-740 740- |
isc moto
tion of d e of 17C A Fixed to Normal Fixed to |
r.
lisc motor is ) to 400 rpn \FCO ) ''H'' operation ) ''L'' |
fed to control speed c
n. APCO Fixed to 50% duty cycle output Normal operation Fixed to 50% duty cycle output |
of | |
15 | 4/1 | I |
FG IN pulse setting. Eithe
set. 4/1 ''H'' level |
r of 1 o |
r 4 pulse pe
FG p disc |
er each rotation can b
rulse per each motor rotation 1 4 |
)e | ||
16 | OVRG | I |
At start
On play, CLV ap |
5 V
0 V plication begins. |
o select v
ol is peri - FG IN |
whether or
formed by F input valid |
not disc motor rotatio
G IN input. |
'n | |
17 | APCG | I | "Н" |
ON/OFF selection input of
trol. "'L'' (generator OFF): Al th th qu pr fre pa Ol |
f APC sin
PC output at is dut e internat Jency ge hase diff equency arison with FF to ON |
gnal genera
ut is fixed to y ratio of 50 al phase cor eneration se erence ''0'' , the start hen the gen I is set to pl |
tor for CLV servo cor
o phase difference ''0' ). At the same time, a mparison reference fre ection is arranged int against the controlle point of phase com erator is changed from mase difference ''0''. |
1-
45 2- 50 4d 1- m |
|
18 | DMLD | 0 |
START †
Lock |
Disc motor lock detection
vo control. Detects the frequency of t is within ±5% deviation, deviation, it is reset. This When set, this flip-flop out to pin APCG, is used for c |
output o
he frame it is set. output s put beco ontrol o |
f AFC signal
e sync signa When the signal is the pmes ''H''. f APC block |
l generator for CLV ser
il. When the frequenc frequency is over ±10 flip-flop output signa This output, connecter |
r-
9 0 1. d |
Pin No. | Symbol | 1/0 | Waveform | Description | Remarks |
---|---|---|---|---|---|
19 | APCO | 0 |
5 V
50 μS 0 V |
APC signal output for CLV servo control.
The output is a PWM (Pulse Width Modulation) wave with resolution = 8 bits, carrier frequency = 8.27 kHz and linear output range = 8 π/9. |
|
20 | AFCO | 0 |
5 V
50 μS 0 V |
AFC signal output for CLV servo control.
The output is a PWM wave with resolution = 8 bits, carrier frequen- cy = 8.27 kHz and linear output range = ±10%. |
|
21 | P/S | I | "Н" | CLV servo control signal ON/OFF input. At play, this pin is set to "H" and, at stop, to "L". This input signal is given the highest priority in the CLV servo control system. When this pin is "L", AFC output is fixed to "L", and APC output gets duty ratio of 50. | |
22 | SCSE | I |
Data selection input for 4 outputs of sub-code signal SCT/T - S/W
''L'' level: Data of 4 bits, P, Q, R and S is output. ''H'' level: Data of 4 bits T, U, V and W is output. |
||
23-26 |
SC P/T
SC Q/U SC R/V SC S/W |
0 | _ |
8-bit data output of sub-code signal P, Q, R, S, T, U, V, W. This signal is the data of each frame. Here, 4-bit data is output by signal SCSE as required. Data selection of each frame is performed in syn-
chronization with the rising edge of signal PFCK. |
Not connected |
27 | V DD | _ | _ | Voltage supply pin. | |
28 | V ss | - | GND pin | ||
29 | S 0 S 1 | 0 | _ | When sub-code signal pattern SO or S1 is detected, this output becomes "H" for that input frame period. | Not connected |
30 | SCPD | 0 |
Output to indicate the date contents of sub-code signal P. Data ob-
tained when the data of each frame is checked in units of 5 frames by the sub-code signal P detection section is output. |
Not connected | |
31 | PFCK | 0 | _ |
The frame period output with duty ratio of 50.
The sub-code data is switched in synchronization with the falling edge of this output. |
Not connected |
Table 2-3-3A
Pin No. | Symbol | 1/0 | Waveform | Description | Remarks |
---|---|---|---|---|---|
32 | QDSS | "H" | Input for sub-code sync pattern detection mode selection, demodulating sub-code signal Q. | ||
33 | QDRD |
QDRD
5 V 5mS 0 V QDRE 13 mS |
Input used in reading the sub-code signal Q data inside internal
memory in units of 4 bits via outputs QDA-a to QDA-d. When signal QDRD becomes "H", the next 4-bit data is set to pins QDA-a to QDA-d after an arbitrary period from that pulse edge. |
||
36 | QDRE | ο |
5 V
5 mS 0 V 13 mS 5 V 5 mV 0 V 13 mS 0 V |
Enable signal output reading sub-code signal Q. When error judge-
ment of 80-bit input sub-code signal Q data is completed, those 4-bit data of MSB side are set to pin QDA-a to QAD-d, and output QDRE becomes "H". When 20 pulses are input to QDRD or when data Q in the next block is written before the data written in internal RAM is read out, output QDRE becomes "L" so that data reading is disabled. |
|
37 | QDAS |
_J LJ I
With block error |
Data selection input for sub-code signal Q data outputs QAD-a to QAD-d. For easier interface with the microprocessor, this input determines output data at QDA-a to b, QDRE and QDE ports. QDAS Port QDAa QDAb QDAc QDAd L QDRE QDAb QDAc L H QDAa QDAb QDAc QDAd | ||
34, 35 | NC | - | Not connected. | ||
38 | QDA-d |
5 V
20 mS 0 V |
The 80-bit sub-code signal Q data, the block error judgement result of
the sub-code signal Q data output or signal QDRE, is output according to the ''L'' or ''H'' setting of QDAS. For data transfer to the |
||
39 | QDA-c | 0 |
5 V
20 mS 0 V |
Inicroprocessor, QDAS is made "L" lifst, then the error judgement
result of data Q is transferred and signal QDRD is input with QDAS "L". Thus, data Q is transferred in units of 4 bits as required. In addition, QDA-a to QDA-d are 3-state outputs, where selection bet- ween output mode and high-impedance mode is made by "L" or "H" of QDSE. |
|
40 | QDA-b | 0 |
5 V
20 mS 0 V |
QDEa QDEb Result of judgement Output data processing H H No error Direct output L H 1-bit error of CRCC Direct output | |
41 | QDA-a |
(Example of wave-
form) |
H L 1-bit error of data Q 1-bit correction output L L Error of 2 bits or more Direct output |
Table 2-3-3A
Pin No. | Symbol | 1/0 | Waveform | Description | Remarks |
---|---|---|---|---|---|
42 | WSEG | Window selection of gate signal which, when the frame sync pattern of EFM signal is detected, determines whether or not this pattern is given as the sync signal for the internal system. WSEG Gate signal window (number of clocks PLCK) L ±3 H ±7 | |||
43 | TMWS | 1 | _ | Selects the number of Tmax = N (PLCK) in detection of T mex of EFM signal which is input from pin EFM2. TMWS N (PLCK) L 11±1 H 11±0.5 | |
44 | FSGM | When no frame sync pattern is detected within the window of the frame sync separation protection gate signal in N continuous frames, system synchronization is made by the next input frame sync pattern without the window. These two inputs are used in selection of number N. FSGL FSGM N (frame) | |||
45 | FSGL | ł | _ | L L 12 H L 8 L H 4 H H 2 | |
46 | TMGS | I | To prevent faulty T max detection, data is valid only when data T max continues N times. This number N is determined by the input. TMGS N L 7 H 4 | ||
47 | NC | _ | _ | Not connected. |
Pin No. | Symbol | 1/0 | Waveform | Description | Remarks |
---|---|---|---|---|---|
The frequency data obtained from Tmax detection of EFM signal which is input from EFM2 is output in one of 3 states as the result of comparison between signal PLCK and Tmax. This output can be used as the frequency status for the PLL circuit.
When P/S signal is "L" (stop mode), output TMO is compulsorily fixed to "H". |
|||||
48 | тмо | о |
''DC 2.5 V''
∼3.0 V |
EFM signal frequency status TMO | |
fTmax>fPLCK L | |||||
fTmax≒fPLCK High impedance | |||||
fTmax>fPLCK H | |||||
49 | QDSE | I | "H" | Input of ''H'' compulsorily makes outputs QDA-a to QDA-d into high impedance state. This input enables effective use of microprocessor input ports. | |
50 | TMOR | I |
This appears when
no synchronization is obtained over some frames. |
Input of "L" compulsorily makes output TMO into high impedance state. Normally, it is connected to FSPS or FSLO. | |
51 | FSPS | ο |
20 mS
5 V 0 V |
Output to indicate the system sync state on the frame sync pattern.
Becomes "H" when no sync pattern is given within the window of gate signal in N continuous frames on selection by input FSGL or FSGM. |
|
52 | EFM2 |
5 V
0.2 µS 0 V |
Input of EFM signal regenerated from disc. The signal obtained by slicing the signal from the RF amp by the level comparator is directly input (asynchronous to signal PLCK). | ||
53 | EFM1 |
4.2 V
0.2 µS 0.4 V 0 V |
Input for EFM signal regenerated from disc. Differently from input signal EFM2, this signal is synchronized to falling edge of signal PLCK phase-locked in the PLL circuit. | ||
54 | PLCK |
4.4 V
0.2 µS 0 V |
Clock pulse input for frame sync separation. This signal is fed from external PLL circuit based on HF signal reproduced from disc. This Clock pulse signal is locked to 4.32 MHz and have duty ratio of 50. |
Pin No. | Symbol | 1/0 | Waveform | Description | Remarks |
---|---|---|---|---|---|
55 | FSLO | 0 |
5 V
2 mS 0 V |
When each system is in synchronization by the frame sync pattern,
and when that input pattern is completely synchronized with the frame sync pattern in internal frame counter (the frame synchroniza- tion necessarily has 588 pulses PLCK), "L" is output during the frame period. |
Not connected |
56 | PBFS | 0 |
5 V
50 μS 140 μS |
When "H" is output with a frame sync signal, demodulation data U 0 to U 31 are transferred to TC9179 (IC6). If "H" which acts as an enable flag, symbol data U 0 to U 31 transfer will be possible by MWRE. |
* Note
Connected to PBFS (pin 2) of TC9179F (IC6) |
57~60
62~65 |
DBOO-
DB07 |
о |
5 V
0.2 μS 0 V |
Outputs for demodulation data U 0 to U 31 in each frame. These are 3-state outputs. When pin BOEN is "L", data is output. DB00 (LSB) to DB07 (MSB) |
* Note
Connected to I/O 0 - 7 (pins 19-26) of TC9179F (IC6) |
66 | BOEN | ł |
5 V
1 μS 0 V 3.8 μS |
Input for enable signal which turns ON the DBOO to BD07 bus driver. |
* Note
Connected to BOEN (pin 4) of TC9179F (IC6) |
67 | MWRE | 0 |
5 V
1 μS 0 V 3 μS |
Output for the enable signal which makes memory write enable.
Becomes "L" at the timing at which data is set to the DBOO to DBO7 data transfer register. When pin BOEN is "H" and it becomes "L" when pin MWRE becomes "H". After signal PBFS becomes "H", it emits 32 outputs every 17 clock pulses PLCK. |
DB00 |
Table 2-3-3A
* Note Data are set to register and MWRE is changed to ''L'' from ''H''. This means data are ready to be written into the external RAM. In this condition, BOEN (''L'' active) from TC9179F turns bus driver on for 8-bit data DB00 to DB07 transfer. At the same time of DB00 to DB07 data transfer, PBFS signal is sent to TC9179AF as a frame sync signal. When PBFS is ''H'', U0 to U31 is output.
2-3-4 IC6 (TC9179F) Error correction
Pin connection
Fig. 2-3-4A
Block diagram
Fig. 2-3-4B TC9179F Block diagram
Pin functions
Pin No. | Symbol | I/O | Waveform | Description | Remarks |
---|---|---|---|---|---|
27, 61 | V DD | _ | Voltage supply pin | ||
28, 62,
67 |
V ss | - | - | GND pin | |
2 | PBFS | I | _ | Frame sync input. The symbol data period signal of each frame sent from TC9178F (IC8) is input. |
Connected to PBFS
(pin 56) of TC9178F (IC8) |
З | MWRE | - |
Memory write request input which accepts MWRE signal from
TC9178F (IC8) |
Connected to MWRE
(pin 67) of TC9178F (IC8) |
|
4 | BOEN | 0 | - |
Output enable. When signal MWRE from TC9178F (IC8) can be ac-
cepted, the control signal to release symbol data output DB00 to DB07 from Hi-impedance state is output. |
Connected to BUSE
(pin 66) of TC9178F (IC8) |
5~14,
18 |
AD0 ~ AD9,
AD10 |
О |
5 V
0.2 μS 0 V |
External RAM address data output, Connected to address data input of external RAM. | |
15 | R/W | О |
5 V
0.2 μS 0 V |
Read/write signal output to external RAM. Connected to R/W input of
external RAM. ''L'' = Read, ''H'' = Write |
|
16 | CE2 | о |
Chip enable 2 signal is output when external RAM is read or written.
Connected to CE2 input of external RAM. |
Not connected | |
17 | CE1 | 0 |
5 V
0.5 μS 0 V 0.48 μS |
Chip enable 1 signal is output when external RAM is read or written.
Connected to CE1 input of external RAM. |
|
19~26 |
1/0-7 ~
1/0-0 |
1/0 |
5 V
0.2 μS 1 μS |
Data bus line connected to I/O-O to 7 of external RAM and DBO4
-DB07. |
92
Pin No. | Symbol | 1/0 | Waveform | Description | Remarks |
---|---|---|---|---|---|
29 | ALGC | _ | Process selection input of C2 correction section. Selects the process algorithm for the frame in which detection of error symbol is not possible in C2 correction section. It is "L" in normal operation. |
Connect to system
GND. (Normal position) |
|
30~33 |
АТ-0
~
АТ-3 |
1/0 |
Digital attenuator I/O controlled by signal WDCK
WDCK = ''L'', outputs internal digital attenuator level WDCK = ''H'', reads external control data for digital attenuator. (AT-3 is not connected.) |
||
34 | MUT-1 | I |
Muting control input of the automatic control section of the internal digital attenuator.
At ''L'', attenuation amount increases (finally, it becomes digital ''0''). At ''H'', attenuation amount decreases (it shifts to 0 dB side). |
||
35 | MUT-01 | 0 | _ | Muting 1 output. Outputs an "L" signal when burst error over 64 frames or buffer-over of jitter absorption memory is detected. | |
36 | MUT-02 | 0 | _ | Muting 2 output. Outputs an "L" signal when deinterleave error is detected over 3 continuous frames. | |
37 | P/S SE | I |
Output data parallel/serial selection input.
''L'' = parallel output, [''H'' = serial output.] |
||
38 | DA-0 | 0 | P/S SE = ''L'' P/S SE ≈ ''H'' Outputs LSB of 8-bit data. Outputs serial data from LSB. | Not connected | |
39 | DA-1 | 0 |
P/S SE = ''L''
P/S SE = ''H''
Outputs the second bit from
LSB of 8-bit data. Outputs correction flag of 8 bits of MSB side. |
Not connected | |
40 | DA-2 | 0 | _ | P/S SE = ''L'' P/S SE = ''H'' Outputs the third bit from LSB of 8-bit data. Outputs correction flag of 8 bits of LSB side. | Not connected |
Pin No. | Symbol | 1/0 | Waveform | Description | Remarks |
---|---|---|---|---|---|
41, 42 | NC | _ | _ | Not connected. | |
43 | DA-3 | 0 | P/S SE = ''L'' P/S SE = ''H'' Outputs the fourth bit from LSB of 8-bit data. Outputs a ''H'' signal when correction flag of LSB side is set side with level of MSB side at -30 dB. | Not connected | |
44 | DA-4 | 0 | _ | P/S SE = ''L'' P/S SE = ''H'' Outputs the fifth bit from LSB of 8-bit data. 1 MCK output. Outputs the clock signal (1.058 MHz) obtained from 2-division of signal CK2M. | Not connected |
45 | DA-5 | 0 | _ | P/S SE = ''L'' P/S SE = ''H'' Outputs the sixth bit from LSB of 8-bit data. APL output. Outputs R-channel aperture signal. | Not connected |
46 | DA-6 | 0 | P/S SE = ''L'' P/S SE = ''H'' Outputs the seventh bit from LSB of 8-bit data. APL output. Outputs L-channel aperture signal. | Not connected | |
47 | DA-7 | 0 |
5 V
0.5 μS 0 V |
P/S SE = ''L'' P/S SE = ''H'' Outputs MSB of 8-bit data. Outputs music data in serial from MSB. | |
48 | ВСК | 0 |
5 V
0.2 μS 0 V |
Bit clock pulse is output when serial data is output. Thus, serial data is
output in synchronization with the rising edge of this clock pulse (1.4 MHz). |
Pin No. | Symbol | 1/0 | Waveform | Description | Remarks |
---|---|---|---|---|---|
49 | MLCK | 0 | MSB/LSB clock pulse output. Outputs the clock signal (176.4 kHz) obtained from 8-division of signal BCK, which is used as a set clock pulse when 8-bit parallel data is output. | Not connected | |
50 | WDCK | 0 |
5 V
5 μS 0 V |
Word clock pulse output. Outputs the clock signal (88.2 kHz) obtained from 16-division of signal BCK, which indicates the output period of one word. | |
51 | L/RG | 0 |
5 V
5 µS 0 V |
Sampling frequency output. Outputs the clock signal (44.1 kHz) ob-
tained from 2-division of signal WDCK, which indicates the data out- put channel. "'L'' = L channel, "'H'' = R channel. |
|
52 | X-0 | 0 |
X'tal OSC connection pins. X'tal OSC is connected to generate the
clock signal required in the system. |
||
53 | X-1 | | | 0.05 μS |
(Feedback resistance and amp incorporated)
X'tal OSC frequency = 8.4672 MHz |
|
54 | CKSE | 1 | _ |
Selection pin which informs X'tal OSC frequency.
(Pullup resistance incorporated) [''H'' or open = 8.4672 MHz, ''L'' = 4.2336 MHz |
|
55 | CK4M | 0 |
5 V
0.2 µS 0 V |
4 MHz clock pulse output. Outputs 4.2336 MHz, which is also used as the clock signal for microprocessor. | |
56 | CK2M | 0 |
5 V
0.2 μS 0 V |
2 MHz clock pulse output. Outputs 2.1162 MHz, which is used as the clock signal for TC9178F (IC8). |
Connected to C21K
(pin 7) of TC9178F (IC8) |
57 | TES1 | Test pins (pullup resistance incorporated) | |||
58 | TES2 | In normal operation, it is "H" or open. | |||
59 | COFS | Ο |
5 V
50 μS 0 V 44 μS 90 μS |
Frame period signal output. Outputs corrected frame period signal. |
Pin No. | Symbol | I/O | Waveform | Description | Remarks |
---|---|---|---|---|---|
60 | DSLP | 0 |
5 V
50 µS 0 V |
Data status signal output. (Error information signal output) | |
63 | DAST | 0 |
5 V
50 μS 0 V 138 μS |
Data status signal output. (Error information signal output) | |
64 | DIV – | 0 |
5 V
0.5 mS 0 V 138 μS |
Buffer memory status output.
Outputs an "H" signal when the jitter absorption buffer memory enters range of +2 or +3 frames in its capacity of ±4 frames. This output is connected to pin DIV- of TC9178F (IC8) to lower the disc motor revolution. |
Connected to DIV –
(pin 5) of TC9178F (IC8) |
65 | DIV + | 0 |
5 V
0.5 mS 0 V 138 μS |
Buffer memory status output.
Outputs an "H" signal when the jitter absorption buffer memory enters range of -2 or -3 frames in its capacity of ±4 frames. This output is connected to pin DIV + of TC9178F (IC8) to raise the disc motor revolution. |
Connected to DIV +
(pin 4) of TC9178F (IC8) |
66 | BUSE |
Buffer selection input pin.
Selects the output condition of DIV – /DIV + . At "H", Div± output are made when the buffer memory enters range of ±2 frames. At "L", Div± output are made when it enters range of ±3 frames. |
Table 2-3-4A
Fig. 2-3-5A
Block diagram
Fig. 2-3-5B
Pin No. | Port name |
Signal
name |
I/O | Initial value | Description | ||
---|---|---|---|---|---|---|---|
9 | RO | SVC (A) | 0 | Output for focus offset amount control data to Q102 (SVC circuit) bit 0 | |||
10 | R1 | SVC (B) | 0 | Output for focus offset amount control data to Q102 (SVC circuit) bit 1 | |||
11 | R2 | SVC (C) | 0 | U | Output for focus offset amount control data to Q102 (SVC circuit) bit 2 | ||
12 | R3 | OF INH | 0 | Output for focus offset amount control data to Q102 (SVC circuit) bit 3 | |||
13 | R4 | TEP | I | 1 |
Input for focus offset amount 1-level shift request signal.
During execution of kick operation, becomes ''L'' to perform 1-level shift. |
||
14 | R5 | RFES | I | 1 |
Input for SVC operation (counting the number of errors) halts request signal.
When track jump occurs, becomes ''H''. After that, stops operation for 1.2 msec. |
||
1 | R6 | CIER | ł | 1 |
Input for block error signal from IC11.
When block error occurs, becomes "H". |
||
2 | R7 | COFS | 1 | 1 |
Input for corrected frame period signal (7.35 kHz square wave) from IC6.
At the point when it becomes "H" signal CIER is judged. |
||
3 | R8 | EOF # | о | 1 |
Output for focus offset amount control data to Q102
(TC4051BP) Not used. bit 1 |
||
4 | R9 | EOF₄ | 0 | 1 | Not used. Grounded. | ||
5 | R10 | STAT | 1/0 | 1 |
SVC operation start/stop control, which is connected to IC15 (TMP4740N).
When a ''H'' signal is input, operation starts, while when a ''L'' signal is input, operation stops. In addition, when offset amount adjustment is complete, it output a ''L'' signal with a duration of 3.4 msec. |
||
6 | R11 | EXSEL | I | 1 | Not used. Grounded. | ||
7 | CK2M | I | Clock pulse input. | ||||
8 | Vss | GND pin | |||||
15 | RESET | I | Initialize signal input. | ||||
16 | _ |
Power
supply |
Power supply (+5 V) pin. |
IC12 (MB88201) is the CPU to control focus offset amount against temperature change, etc. (This control operation is termed SVC operation for short.)
Focus offset amount is controlled by control of bilateral switch Q102 (TC4051BP) through SVC (A) ≅ SVC (C) and OFINH. The following table shows the relationship between each ports and offset level.
Ports
Level |
OFINH | SVC (A) | SVC (B) | SVC (C) | Remarks |
---|---|---|---|---|---|
2 | 0 | 0 | 1 | 0 | |
1 | 0 | 1 | 0 | 0 | |
0 | 0 | 0 | 0 | 0 | Initial select offset level |
7 | 0 | 1 | 1 | 1 | |
6 | 0 | 0 | 1 | 1 | |
5 | 0 | 1 | 0 | 1 | |
4 | 0 | 0 | 0 | 1 | |
3 | 0 | 1 | 1 | 0 | |
INH | 1 | × | × | × |
x : Don't care
As shown in the table, the offset level can be set to 8 levels. The offset level is determined by the amount of NFB to the focus error amp Q103, i.e. the value of resistor is changed by bilateral switch controlled by SVC (A) to (C), OFINH. The following outlines the focus offset amount adjustment procedure.
Fig. 2-3-5C shows that, starting from the initial offset level, counting of number of block errors executed from level 0. The offset level is stepped down one by one till the count exceeds 2000 (in this case N=A>2000 at level 3). From the level of which the count exceeded 2000, the offset level is stepped up 3 levels (in this case to level 6: N=B) for enough clearance margin for block error numbers. This level is maintained till the end of playback unless the disc is changed or stopped.
For counting of the number of block errors, the number of times by which block error signal CIER from IC11 (TC4094BP) generated in synchronization with correction frame period signal COFS (7.35 kHz square wave) from IC6 (TC9179F) becomes "H" is counted.
Measurement of the number of block errors at each offset level is done by 256 x 6 samples (rising edges of signal COFS). Normally, this measurement is completed in approx. 0.2 sec. In addition, when signal RFES becomes "H" (when track jump occurs), the measurement is halted for approx. 1.2 msec.
Start and stop of this SVC adjustment operation is controlled by IC15 (TMP4740N). In this case, when STAT becomes "H", this operation starts, while when it becomes "L", the operation stops and focus offset amount returns to the set value before adjustment. Further, when the operation is complete, STAT outputs an "L" signal with a duration of about 3.4 msec to inform IC15 (TMP4740N) of completion.
Fig. 2-3-5D
2-3-6 IC14 (TC5514P) T.O.C. Memory
Pin connection diagram
Fig. 2-3-6A
Pin functions of external RAM IC14 (TC5514P)
Pin
No. |
Port pin
name |
Signal
name |
1/0 |
Initial
value |
Description | |
---|---|---|---|---|---|---|
5 | AO | AO | I | Address input from IC15 (TC4740N) (X32-1010-11) | bit 0 | |
6 | A1 | A1 | Ι | Address input from IC15 (TC4740N) (X32-1010-11) | bit 1 | |
7 | A2 | A2 | I | Address input from IC15 (TC4740N) (X32-1010-11) | bit 2 | |
4 | A3 | A3 | 1 | Address input from IC15 (TC4740N) (X32-1010-11) | bit 3 | |
3 | A4 | A4 | Ι | * | Address input from IC15 (TC4740N) (X32-1010-11) | bit 4 |
2 | A5 | A5 | Ĩ | Address input from IC15 (TC4740N) (X32-1010-11) | bit 5 | |
1 | A6 | A6 | Ĩ | Address input from IC15 (TC4740N) (X32-1010-11) | bit 6 | |
17 | A7 | A7 | Address input from IC15 (TC4740N) (X32-1010-11) | bit 7 | ||
16 | A8 | A8 | I | Address input from IC15 (TC4740N) (X32-1010-11) | bit 8 | |
15 | A9 | A9 | 1 | Address input from IC15 (TC4740N) (X32-1010-11) | bit 9 | |
14 | I/01 | D0 | I | Data in/output from IC15 (TC4740N) (X32-1010-11) | bit 0 | |
13 | 1/02 | D1 | 1/0 | Data in/output from IC15 (TC4740N) (X32-1010-11) | bit 1 | |
12 | 1/03 | D2 | 1/0 | Data in/output from IC15 (TC4740N) (X32-1010-11) | bit 2 | |
11 | 1/04 | D3 | 1/0 | Data in/output from IC15 (TC4740N) (X32-1010-11) | bit 3 | |
10 | R/W | I | 1 | Read/write control signal input. "H" = Read, "L" = Write | ||
8 | CE | 1 | Chip enable signal input (active "L") | |||
9 | GND | Ground | Ground | |||
18 | V DD | Power supply | Power supply pin (+5 V) |
The external RAM is provided with the following data storage areas. Different data are written or read by control of microprocessor ports R6, P1 and R5 (R52, R53) (address designation), port R7 (data I/0), port P2 (P20) (write/read control) or port P2 (P21) (chip enable). (Refer to "Pin functions of IC15", Table 2-3-1A.)
First, the method of access to the area of read-in data (Area (1)) is described.
As shown in Table 2-3-6A, IC14 is so configured that row address is designated by microprocessor ports R52 and R53, LSB data of column address by 4 ports R6, and MSB data of column address by 4 ports P1. Here, the microprocessor is programmed so that the binary conversion value of the point data (tune No.) which is read, in reading the lead-in data, is set as column address. A compact disc can record up to a maximum of 99 tunes. Thus, area of column addresses H'01 to H'63 (H' before the number or alphabet means that they are expressed in hexadecimal) is used as save area of lead-in
data (Area (1)). (read-out start time data is saved in code address H'64.)
In combination with the column address determined in this manner, the 10's digit of minutes data of play start time is saved in address 0 of the row address given by ports R52 and R53, the 1's digit of minutes data is saved in address 1, the 10's digit of seconds data in address 2, and the 1' digit of seconds data in location 3. This operation timing is shown in Fig. 2-3-6B. The remaining three areas (2), (3) and (4) relate with preset channels. For channel presetting, a data save area for 16 channels is needed. To meet this need, the area of column addresses H'80 -H'FF is divided into 16 sections. As shown in Table 2-3-6B, four words of index LSB data, index MSB data, TNO LSB data and TNO MSB data (Area (2)) are saved in row address 0 in order from the head column address of each section, four words of 1's digit of seconds data. 10's digit seconds data, 1's digit of minutes data and 10's digit of minutes data (Area (3)) are in row address 1, and five words of 1's digit of seconds data, 10's digit of seconds digit data, 1's digit of minutes data, 10's digit minutes data and 100's digit of minutes data (Area (4)) are in row address 3. Fig. 2-3-6C shows this operation timing.
External RAM IC14 (TC5514P) map
RAM capacity, 1023 words Capacity used, 626 words _____→4 bit
Column address | _ | |||||
---|---|---|---|---|---|---|
R1 | R6 | 0 | 1 | 2 | 3 | |
0 | 0 | |||||
0 | 1 | 10 MIN | 1 MIN | 10 SEC | 1 SEC | TNO. 1 |
0 | 2 | 10 MIN | 1 MIN | 10 SEC | 1 SEC | TNO. 2 |
6 | 2 | 10 MIN | 1 MIN | 10 SEC | 1 SEC | TNO. 98 |
6 | 3 | 10 MIN | 1 MIN | 10 SEC | 1 SEC | TNO. 99 |
6 | 4 | 10 MIN | 1 MIN | 10 SEC | 1 SEC | Read-out start time |
6
≀ 7 |
5
∼ 8 |
|||||
7 | 9 | Upueed | CH CNTL | |||
7 | А | Onuseu | CH CNTH | Number of memories | ||
8 | 0 | INDEX L | 1 SEC | 1 SEC | ||
8 | 1 | INDEX H | 10 SEC | 10 SEC | ||
8 | 2 | TNO. L | 1 MIN | 1 MIN | 0111 | |
8 | 3 | TNO. H | 10 MIN | 10 MIN | llowed | CH DATA |
8 | 4 | 100 MIN | Unused | |||
8 | 5 | Linu | and | Unused | TOTAL TIME | |
8 | 6 | Und | sea | |||
8 | 7 | |||||
8 | 8 | INDEX L | 1 SEC | 1 SEC | ||
8 | 9 | INDEX H | 10 SEC | 10 SEC | ||
8 | А | TNO. L | 1 MIN | 1 MIN | ||
8 | В | TNO. H | 10 MIN | 10 MIN | 011.0 | |
8 | С | 100 MIN | CH 2 | |||
8 | D | linuard | Ununged | |||
8 | E | Unusea | Unused | Unused | ||
8 | F | |||||
9 | 0 | СН 3 | ||||
۲ | 1 | The sar | ne as in 8-8 to 8-F is re | peated. | Unused | |
F | F | CH 16 |
<CH DATA>
<CH TIME> <TOTAL TIME>
The operation timing when play start time data of 53 min 41 sec is written on the point data of tune 20 which is read out in reading the read-in data.