All rights reserved. Reproduction in whole or in part is prohibited without the prior written consent of the copyright
owner. The information presented in this document does not form part of any quotation or contract, is believed to be
accurate and reliable and may be changed without notice. No liability will be accepted by the publisher for any
consequence of its use. Publication thereof does not convey nor imply any license under patent - or other industrial or
intellectual property rights.
Date of release: October 2004
Figure 2 shows a typical application circuit for the BGA2715-17 MM IC.
The device is internally matched to 50 O, and therefore does not need any external
matching. The value of the input and output DC blocking capacitors C2 and C3 should
not be more than 100 pF for applications above 100 MHz. However, when the device is
operated below 100 MHz, the capacitor value should be increased.
The 22 nF supply decoupling capacitor C1 should be located as close as possible to
the MMIC.
The PCB top ground plane, connected to the pins 2, 4 and 5 must be as close as
possible to the MMIC, preferably also below the MMIC. When using via holes, use
multiple via holes, as close as possible to the MMIC.
Table 2 component selection for different frequencies.
V
depends on R
supply
used. Device voltage must be approximately 4 V (i.e. device
bias
current = 80mA).
With formula 1 it is possible to operate the device under different supply voltages.
If the temperature raises the device will draw more current, the voltage drop over Rbias
will increase and the device voltage decrease, this mechanism provides DC stability.
Measured small signal performance.
Small signal performance BGA6289
20.00
15.00
10.00
5.00
0.00
0.00500.001000.001500.002000.002500.003000.00
-5.00
-10.00
-15.00
-20.00
-25.00
-30.00
f [MHz]
Figure 2 Small signal performance.
Measured large signal performance.
f 850 MHz 2500 MHz
IP3
31 dBm 25 dBm
out
PL
18 dBm 16 dBm
1dB
NF 3.8 4.1
Table 3 Large signal performance and noise figure.
Table 2 component selection for different frequencies.
V
depends on R
supply
used. Device voltage must be approximately 5.1 V (i.e. device
bias
current = 80mA).
With formula 1 it is possible to operat e the device under different supply voltages.
If the temperature raises the device will draw more current, the voltage drop over Rbias
will increase and the device voltage decrease, this mechanism provides DC stability.
Measured small signal performance.
Figure 2 Small signal performance.
Small signal performance BGA6489
30.00
20.00
10.00
0.00
0.00500.001000.001500.002000.002500.003000.00
-10.00
-20.00
-30.00
-40.00
f [MHz]
S11
S12
S21
Measured large signal performance.
f 850 MHz 2500 MHz
IP3
33 dBm 27 dBm
out
PL
20 dBm 17 dBm
1dB
NF 3.1 dB 3.4 dB
Table 3 Large signal performance and noise figure.
Table 2 component selection for different frequencies.
V
depends on R
supply
used. Device voltage must be approximately 4.8 V (i.e. device
bias
current = 83mA).
With form ula 1 it is possible to operate the device under different supply voltages.
If the temperature raises the device will draw more current, the voltage drop over Rbias
will increase and the device voltage decrease, this mechanism provides DC stability.
Measured small signal performance.
Small signal performance BGA6589
30.00
20.00
10.00
0.00
0.00500.001000.001500.002000.002500.003000.00
-10.00
-20.00
-30.00
-40.00
-50.00
f [MHz]
S11
S12
S21
S22
Figure 2 Small signal performance.
Measured large signal performance.
f 850 MHz 2500 MHz
IP3
33 dBm 32 dBm
out
PL
21 dBm 19 dBm
1dB
NF 3.1 dB 3.4 dB
Table 3 Large signal performance and noise figure.
Due to shrinking of the mechanical dimensions and attractive pricing of the
semiconductors, GPS applications got very popular in the last years. A GPS navigation
system is based on measuring and evaluating RF signals transmitted by the GPS
satellites. There are at least 24 active satellites necessary in a distance of 20200km
above the Earth surface. All sat’s transmits their civil useable L1 signal at the same
time down to the user on 1575.42MHz in the so-called microwave L-band. Each
satellite have it’s own C/A code (Coarse Acquisition).
The GPS Satellites are 20020km far from the Earth surface
The L1 carrier based GPS system does use : CDMA - DSSS - BPSK modulation
Available GPS carrier frequencies
L1 Link 1 carrier frequency 1575.42 MHz
L2 Link 2 carrier frequency 1227.6 MHz
L3 Link 3 carrier frequency 1381.05 MHz
L4 Link 4 carrier frequency 1379.913 MHz
L5 Link 5 carrier frequency 1176.45 MHz
The U.S. navigation system GPS was originally started by the U.S. military in 1979. It will be updated in
order to supply the carriers L2 & L5 for increasing civil performances together with the standard L1 RF
carrier. GPS uses BPSK modulation on the L1 carrier and, beginning with launch of the modernized
Block IIR the L2 carrier. The L5 signal that will appear with the Block IIF satellites in 2006 will have use of
the QPSK modulation (Quadrature Phase Shift Keying).
Randomly and appears like Noise in the
frequency spectrum (= PRN C/A code). The L1
carrier is BPSK (Binary Phase Shift Keying)
modulated by the C/A data code, by the
navigation data message and the encrypted
P(Y)-code. Due to C/A’s PRN modulation, the
carrier is DSSS modulated (Direct Sequence
Spread Spectrum modulation). This DSSS
spreads the former bandwidth signal to a satel
internal limited width of 30MHz. A GPS receiver
must know the C/A code of each satellite for
selecting it out of the antennas kept RF
spectrum. Because a satellite is selected out of
the data stream by the use of an identification
code, GPS is a CDMA-System (Code Division
Multiplex Access). This RF signal is transmitted
Page 16
Philips Semiconductors
RF Manual
APPENDIX
Product and design manual for RF Products
The spread spectrum modulated signals
(
)
The performances overview of the actual and the next up-coming GPS system:
Need of a
Topic Used Codes
Today basic
positioning
Tomorrow basic
positioning
Today advance
positioning
Tomorrow
advanced
positioning
In 2004 will be start the European navigation system EGNOS. News forecasted the European system
Galileo for 2008. GLONA SS is a Russian Navigation System.
All GPS satellites use the same L1 frequency of 1575.42MHz, but different C/A codes, so a single front end may be used. To achieve better sky covera ge and accelerated operation, more than one antenna
can be used. In this case, separate front -ends can be used. Using switches based on Philips’ PIN-diodes
makes it possible to select the antenna with the best signal in e.g. automotive applications for ope ration
in a city.
Each GLONASS satellite will use a different carrier frequency in the range of 1602.5625MHz to
1615.5MHz, with 562.5KHz spacing, but all with the same spreading code. The normal method for
receiving these signals uses of several parallel working front-ends, perhaps with a common first LNA and
mixer, but certainly with different final local oscillators and IF mixer.
Comparison of the front-ends used in a GPS and in a GLONASS receiver:
C/A Code on L1 No
C/A Code on L1
L2C Code on L2
New Code on L5
L1 Code and
Carrier
L2 Carrier
Data Link
L1 Code and
Carrier
L2 Code and
Carrier
L5 Code and
Carrier
Data Link
Competition Satellite based navigation systems:
second
reference base
station
No 1-5m
Yes 2cm
Yes 2cm
Resolution Comments
Before May 2000: 25-
100m Today 6-10m
(resolution controlled
by US)
5th edition
- - -
Eliminates need for
costly DGPS in many
non-safety
applications.
max. distance too
reference 10km
max. distance too
reference 100km;
faster recovery
following signal
interruption
field strength is very weak and cause a
negative SNR in the receiver input
circuit caused by the Nyquist Noise
determined by the Analog Front -End IF
bandwidth:
Satellite
Generation
II/IIA/IIR
IIR-M/IIF
dBW
Channel
L1 -158.5dBW
L2 -164.5dBW
L1 -158.5dBW
L2 -160.0dBW
log10=
C/A
Loop peek
P
W
1
Page 17
Philips Semiconductors
RF Manual
APPENDIX
Product and design manual for RF Products
Avionics
Survey /
Car Navigation
Military
Marine
Tracking /
Application examples:
5th edition
GPS Marked & Applications
- Personal Navigations
- Railroads
- Recreation, walking-tour
- Off shore Drilling
- Satellite Ops. Ephemeris Timing
- Surveying & Mapping
- Network Timing,
Synchronization
- Fishing & Boat
- Arm Clocks
- Laptops and Palms
- Mobiles
- Child safety
- Car navigation systems
- Fleet management systems
- Telecom Time reference
- High way toll system
- First-Aid call via mobiles
OEM
Machine
Control
Mapping
Marked of GPS Applications
Consumer
References:
- Office of Space Commercialization, United States Department of Commerce
- U.S. Coast Guard Navigation Center of Excellence
- NAVSTAR Global Positioning System
- NAVSTAR GPS USER EQUIPMENT INTRODUCTION
- Royal school of Artillery, Basic science & technology section, BST, gunnery careers courses, the
NAVSTAR Global Positioning System
, …
Simplified block diagram of a typically GPS receiver analog front-end IC
Typically, an integrated double superheat -receiver technology is used in the analog rail. The under
sampling analog to digital converter (ADC) is integrated in the analog front -end IC with a resolution of 1
to 2bit. Due to under sampling, it acts as the third mixer for down converting into to the digital stream IF
band. Behind this ADC, the digital Baseband Processor is located. Till this location, the SNR of the
received satellite signals is negative. In the Baseband Processor, the digital IF signal is parallel
processed in several C/A correlators and NAV -data code discriminators. During this processing, the
effective Nyquest Bandwidth is shrink down to few Hertz, dispreading and decoding of the GPS signal is
made causing a positive SNR. Because typically front -end ICs are designed in a high-integrated low
power relative noisy semiconductor process, there is a need of an external Low-Noise-Amplifier (LNA)
combined with band pass-filters. Because the available GPS IC chipsets on the market differ in their
electrically performances like, Gain, Noise Figure (NF), linearity and sensitivity, therefore one and two stage discrete front-end amplifiers are used. The numbers of filters in the front -end vary with the needs
on the applications target environment, costs and sizes. The processed number of GPS carriers as well
as the navigation accuracy does determine the min. allowed band width of the analog-front end rail.
Philips Semiconductors offer MMICs with internal 50Ω matches at the input and output (I/O) and without
internal matching. The internal matched broadband MMICs typically need an output inductor for DC
biasing and DC decoupling capacitors at the amplifier I/O. The internal non -matched devices need I/O
matching network typically made by lumped LC circuits in a L-arrangement. This gives additionally
selectivity. Another advantage of this MMIC is the integrated temperature compensation in contrast to a
transistor. In a system, typically the first amplifier’s noise figure is very important. E.g. the BGU2003 SiGe
MMIC offers both (NF+IP3) with a good quality. It’s Si made brother BGA2003 come with lower amount
of IP3 and NF. IC chip -sets with a need of high front-end gain made by one MMIC may be able to use
BGM1011 or BGM1013. Two-stage design e.g. will use BGA2001, BGA2011 eventually combined with
BGA2748 or BGA2715 or BGA2717. Some examples of configuration for an L1 -carrier LNA are shown in
the next two tables.
Note: [1] Gain=|S21|2; data @ 1.8GHz or the next one / approximated, found in the data sheet /
diagrams
[2] For cascaded amplifier equations referee to e.g. 4th Edition RF Manual Appendix, 2.4GHz
Generic Front -End reference design
[3] The evaluated cascaded amplifier includes an example interstage filter with 3dB insertion loss
(NF=+3dB; IP3=+40dBm).
This note describes the design and realization of a 2.4GHz ISM front end (Industrial-
Scientific-Medical). Useful for wireless communication applications, LAN and e.g.
Video/TV signal transmission. It covers power amplifier (PA) design in the Tx path, Low
Noise Amplifier (LNA) design in the Rx path and RF multiplexing towards the antenna.
Though actual IC processes enable front-end integration to a certain extend, situations
do exists were dedicated discrete design is required, e.g. to realize specific output
power. On top of the factual design, attention is paid to interfacing the front end to
existing Philips IC. More then trying to fit a target application, our intention here is to
illustrate generic discrete Front end design methodology.
Board
§ The job of the Front-End in an application
The board supports half duplex operation. This means the TX and RX operation are not
possible at the same time. The time during TX and RX activity are so called time slots
or just slots. The order of the TX and RX slots is specific for the selected standard.
Special handshaking activities consist of several TX and RX slots put together in to the
so-called time-frame or just frame. The user points / access points linked in this
wireless application must follow the same functionality of slots, same order of frames
and timing procedure (synchronization). These kind of issues must be under the
control of specific rules (standard) normally defined by Institutes or Organization like
ETSI, IEEE, NIST, FCC, CEPT, and so on.
Applications for the Reference Board
Some application ideas for the use of the Generic Front -End Reference Board
§ 2.4GHz WLAN
§ Wireless video, TV and remote control signal transmission
§ PC to PC data connection
§ PC headsets
§ PC wireless mouse, key board, and printer
§ Palm to PC, Keyboard, Printer connectivity
§ Supervision TV camera signal transmission
§ Wireless loudspeakers
§ Robotics
§ Short range underground walky-talky
§ Short range snow and stone avalanche person detector
§ Wireless control of soft -drink /cigarette/snag - SB machine
§ Communication between bus/taxi and the stop lights
§ Panel for ware house stock counting
§ Printers
§ Mobiles
§ Wireless LCD Display
§ Remote control
§ Cordless Mouse
§ Automotive, Consumer, Communication
Please note:
The used MMICs and PIN diodes can be used in other frequency ranges e.g. 300MHz to 3GHz for
applications like communication, networking and ISM too.
Orbcomm Satellite (LEO) eg. GPSS-GSM Satellite 2250,5MHz
Ariane 4 and Ariane 5 (ESA, Arianespace) tracking data link for rocket 2206MHz
Atlas Centaur eg. carrier for Intelsat IVA F4 tracking data link for rocket 2210,5MHz
J.S. Marshall Radar Observatory 700KW Klystron TX S-Band
Raytheon ASR -10SS Mk2 Series S-Band
Solid-State Primary Surveillance Radar
Phase 3D; Amateur Radio Satellite; 146MHz,
436MHz, 2400MHz
Apollo 14-17; NASA space mission transponder experiments S-Band
ISS; (internal Intercom System of the ISS
station)
MSS Downlink UMTS 2170 2200
Standardization name/
issue
IEEE802.15.3 (camera,
video)
IEEE802.15.4
FDD Uplink (D)
FDD Downlink (D)
TDD (D)
ERC, CEPT Band Plan 2400MHz 2450MHz 2425MHz 50/
Amateur Radio Satellite UO11
Amateur Radio Satellite AO16
Amateur Radio Satellite DO17
Satellite; Supplier
Constellation
US FAA/DoD ASR -11
used in U.S. DASR program
AMSAT; 250Wpep TX S-Band 2.4KHz, SSB
Space 2.4GHz
Start frequency Stop Frequency
NUS/EU=2402MHz
(All)=2402MHz
2.4GHz 2.49GHz 2.45GHz
US=2402MHz
EU=2412MHz
≈1920 ≈1980
≈2110 ≈2170
≈1900 ≈2024
NUS/EU=2402MHz
(All)=2402
2401.5MHz
2401.1428MHz
2401.2205MHz
2483.5MHz 2500MHz
2700 2900
NUS/EU=2480MHz
(All)=2495MHz
US=2480MHz
EU=2472MHz
NUS/EU=2480MHz
(All)=2495
Centre
frequency
2442.5MHz
2441MHz
Exact Frequency
range depending on
country & system
supplier
S-Band
S-Band Radar
≈2400MHz
Abbreviations: European Radio communication Committee (ERC) within the European Conference of Postal and Telecommunication
Administration (CEPT)
WPLAN = Wireless Personal Area Networks
WLAN = Wireless Local Area Networks
ISM = Industrial Scientific Medical
LAN = Local Area Network
IEEE = Institute of Electrical and Electronic Engineers
= Short Range Device
RLAN = Radio Local Area Network
ISS =International Space Station
IMT = International mobile Telecommunications at 2000MHz
MSS = Mobile Satellite Service
W-CDMA =Wideband-CDMA
GMSK = Gaussian Minimum Shift Keying
UMTS = Universal Mobile Telecommunication System
UWC = Universal Wireless Communication
MSS Downlink = Mobile Satellite Service of UMTS
RFID
OSCAR = Orbit Satellite Carry Amateur Radio
FHSS = Frequency Hopping Spread Spectrum
DSSS = Direct Sequence Spread Spectrum
DECT = Digital Enhanced Cordless Telecommunications
= North America
EU = Europe
ITU = International Telecommunications Union
ITU-R = ITU Radio communication sector
(D) = Germany
TDD = Time Division Multiplex
FDD = Frequency Division Multiplex
TDMA = Time Division Multiplex Access
CDMA = Code Division Multiplex Access
2G = Mobile Systems GSM, DCS
3G = IMT-2000
1.3 RF Front-End
For: Function of an antenna, examples of PCB design, Transistor Semiconductor Process, see
RF Manual 4th edition on the RF Manual website.
1.1 Frequency spectrum
Radio spectrum and wavelengths
Each material’s composition creates a unique pattern in the radiation emitted.
This can be classified in the “frequency” and “wavelength” of the emitted radiation.
As electro-magnetic (EM) signals travel with the speed of light, they do have the character of
propagation waves.
A survey of the frequency bands and related wavelengths:
Band Frequency
Definition
(English)
VLF 3kHz to 30kHz Very Low Frequency
LF 30kHz to 300kHz Low Frequency
MF 300kHz to 1650kHz Medium Frequency
1605KHz to 4000KHz
Boundary Wave Grenzwellen
HF 3MHz to 30MHz High Frequency
VHF 30MHz to 300MHz Very High Frequency
UHF 300MHz to 3GHz Ultra High Frequency Dezimeterwellen 1m to 10cm 9
SHF 3GHz to 30GHz Super High Frequency Zentimeterwellen 10cm to 1cm 10
EHF 30GHz to 300GHz Extremely High Frequency Millimeterwellen 1cm to 1mm 11
--- 300GHz to 3THz --- Dezimillimeterwellen 1mm-100µm 12
Definition
(German)
Längswellen
(Myriameterwellen)
Langwelle
(Kilometerwellen)
Mittelwelle
(Hektometerwellen)
Kurzwelle
(Dekameterwellen)
Ultrakurzwellen
(Meterwellen)
Wavelength - λ
acc. DIN40015
CCIR Band
100km to 10km 4
10km to 1km 5
1km to 100m 6
100m to 10m 7
10m to 1m 8
Literature researches according to the Microwave’s sub-bands showed a lot of different definitions with
very few or none description of the area of validity. Due to it, the following table will try to give an
overview but can’t act as a reference.
Source Nührmann Nührmann www.wer-
Validity IEEE Radar
Standard 521
Band GHz GHz GHz GHz GHz GHz GHz
A 0,1-0,225
C 4-8 3,95-5,8 5-6 4-8 4-8 4-8 3,95-5,8
D 1-3
For: Fundamentals and RF Amplifier design Fundamentals, download RF Manual 4th edition on the RF
Manual website.
Small signal RF amplifier parameters
1. Transistor parameters, DC to microwave
At low DC currents and voltages, one can assume a transistor acts like a voltage-controlled current
source with diode clamping action in the base-emitter input circuit. In this model, the transistor is
specified by its large signal DC-parameters, i.e., DC-current gain (B, ß, hfe), maximum power
dissipation, breakdown voltages and so forth.
U
BE
V
T
eII⋅=
COC
Thermal Voltage: VT=kT/q≈26mV@25°C
ICO=Collector reverse saturation current
Low frequency voltage gain:
I
Current gain
C
ß =
I
r ='
e
V ≈
B
V
T
I
E
R
C
u
'
r
e
Increasing the frequency to the audio frequency range, the transistor’s parameters get frequency dependent phase shift and parasitic capacitance effects. For characterization of these effects, small
signal h-parameters are used. These hybrid parameters are determined by measuring voltage and
current at one terminal and by the use of open or short (standards) at the other port.
The h-parameter matrix is shown below.
h-Parameter Matrix:
u
1
=
i
2
hh
1211
hh
2221
i
1
∗
u
2
Increasing the frequency to the HF and VHF ranges, open ports become inaccurate due to electrically
stray field radiation. This results in unacceptable errors. Due to this phenomenon y-parameters were
developed. They again measure voltage and current, but use of only a “short” standard. This “short”
approach yields more accu rate results in this frequency region. The y-parameter matrix is shown
below.
Further increasing the frequency, the parasitic inductance of a “short” causes problem due to
mechanical depending parasitic. Additionally, measuring voltage, current and it’s phase is quite tricky.
The scattering parameters, or S-parameters, were developed based on the measurement of the
forward and backward traveling waves to determine the reflection coefficients on a transistor’s
terminals (or ports). The S-parameter matrix is shown below.
S-Parameter Matrix:
b
1
=
b
2
SS
SS
a
1211
2221
1
∗
a
2
2. Definition of the S-Parameters
Every amplifier has an input port and an output port (a 2-port network). Typically the input port is
labeled Port-1 and the output is labeled Port-2.
Matrix:
Equation:
b
1
=
b
2
SS
SS
Figure 10: Two-port Network’s (a) and (b) waves
The forward-traveling waves (a) are traveling into the DUT’s (input or output) ports.
The backward-traveling waves (b) are reflected back from the DUT’s ports
The expression “port ZO terminate” means the use of a 50Ω-standard. This is not a conjugate complex
power match! In the previous chapter the reflection coefficient was defined as:
Reflection coefficient:
r =
ng waveback runni
nning waveforward ru
b
Calculating the input reflection factor on port 1:
S
That means the source injects a forward-traveling wave (a1) into Port-1. No forward-traveling power
(a2) injected into Port-2. The same procedure can be done at Port-2 with the
b
Output reflection factor:
S
2
with the input terminated in ZO.
22
0
==a
1
a
2
waveoutput
Gain is defined by:
gain
=
waveinput
The forward-traveling wave gain is calculated by the wave (b2) traveling out off Port-2 divided by the
wave (a1) injected into Port-1.
The backward traveling wave gain is calculated by the wave (b1) traveling out off Port-1 divided by
b
the wave (a2) injected into Port-2.
The normalized waves (a) and (b) are defined as:
1
a
2
a
2
b
2
b
2
()
Z
O
1
()
Z
O
1
()
Z
O
1
()
Z
O
iZV
⋅+== signal into Port-1
111
O
iZV
⋅+== signal into Port-2
222
O
iZV
⋅+== signal out of Port-1
111
O
iZV
⋅+== signal out of Port-2
212
O
S
The normalized waves have units of tWat and are
1
12
0
==a
1
a
2
dBS20logFT21=
Isolation:
dBS20logS12(dB)12−=
Input Return Loss:
−=
dBS20logRL
11in
Output Return Loss:
−=
dBS20logRL
22OUT
Insertion Loss:
dBS20logIL21−=
referenced to the system impedance ZO. It is shown by
the following mathematical analyses:
The relationship between U, P an ZO can be written as:
u
Z
O
a
V
1
+=
Z
O
ZiP
⋅==Substituting:
O
iZ
⋅
O
Z
22
O
P
11
1
+=
2
iZ
⋅
O
1
Z
2
O
Z
0
Z
Z
=
O
O
Rem:
Z
O
Z
ZZ
⋅
U
OO
ZZ
⋅
OO
2
=
O
IUP
=⋅=èRI
R
⋅
=
Z
U
P⋅==
R
ZZ
OO
Z
=
O
O
⋅
a
1
Because
O
+=è
V
forward
a =
1
, the normalized waves can be determined the measuring the voltage of a
Z
O
forward-traveling wave referenced to the system impedance constant
PPiZP
1111
+=
2222
Pa = (è Unit =
11
Watt =)
Volt
Ohm
Z . Directional couplers or
O
VSWR bridges can divide the standing waves into the forward- and backward-traveling voltage wave.
(Diode) Detectors convert these waves to the V
forward
and V
backward
DC voltage. After an easy
processing of both DC voltages, the VSWR can be read.
V
forward
V
backward
50Ω VHF-SWR-Meter built from a kit (Nuova Elettronica). It
consists of three strip-lines. The middle line passes the main
signal from the input to the output. The upper and lower striplines select a part of the forward and backward traveling waves
by special electrical and magnetic cross-coupling. Diode
detectors at each coupled strip-line-end rectify the power to a
DC voltage, which is passed to an external analog circuit for
processing and monitoring of the VSWR. Applications: Power
antenna match control, PA output power detector, vector
voltmeter, vector network analysis, AGC, etc. These kinds of
circuit’s kits are published in amateur radio literature and in
written consent of the copyright owner. The information presented in this document does
be changed without notice. No liability will be accepted by the publisher for any
consequence of its use. Publication thereof does not convey nor imply any license under
patent- or other industrial or intellectual property rights.
Document
Published in The Netherlands
Loading...
+ hidden pages
You need points to download manuals.
1 point = 1 manual.
You can buy points or you can get point for every manual you upload.