Dahua NAVIGATOR X1100 User Manual
NAVIGATOR X1100
User’s Manual
V1.0.0
ZHEJIANG DAHUA VISION TECHNOLOGY CO.,LT D
Copyright
© 2018 ZHEJIANG DAHUA VISION TECHNOLOGY CO.,LTD. All rights reserved.
Any or full contents of the user’s manual cannot be copied, transmitted, distributed, partially or
wholly, by any means, without the prior written notice of ZHEJIANG DAHUA VISION
TECHNOLOGY CO.,LTD.
Dahua or the third party may reserve the right of the product described in this user’s manual.
Without the prior written approval of the corresponding party, any person cannot (including but
not limited to) copy, distribute, amend, excer pt , r everse compile, disassemble, decode, reverse
engineering, rent, tr ansfer or sublicense the software.
Legal Statement
Trademark
, , and are the trademarks or registered
trademarks of Dahua and its branch companies in various jurisdictions. Other trademarks or
company names mention ed ar e t he pr operties of their respective owner s.
Update and Modification
In order to enhance the product security and provide better user experience, Dahua may
improve the product via software auto update, but Dahua doesn't need to inform in
advance and isn't liable to any responsibility.
Dahua reserves the right to modify any information in this document at any time; the
modified contents will be added to the new version without prior announcement. There
may be minor differences about some product functi ons after it is updated.
I
Document Overview
No.
Name
Product
It is to introduce the function features and ap plicatio n scenarios o f the
It is to comprehensively introduce main components of the prod uct.
Read the chapter before use; understand product structure and
application methods of m ain components.
It is to elaborate the complete f low of aircraft unlock before ta keoff.
Strictly conform to the installation debugging sequence of the
chapter, install each component and make initial debugging before
If it is not the first time to use the device, you can select the
However, confirm that all the components (unnecessary steps
excluded) listed in the chapter have been stably installed. Please
chapter; the operation seq uence can't be reversed.
The manual is to comprehensively introduce function features, structure parameters,
installation, dismounti ng and flight guide etc. of the product.
Applied Model
X1100
Application Object
Preface
End users.
Reading Guide
Chapter
1
2
3
Chapter
Overview
Product
Component
Flight
Preparation
Main Content
product.
first use.
installation content according to the dismounting situation last time.
conform to the operating steps in this chapter strictly and follow the
operating sequence.
It is to elaborate the complete flow of aircraft formal launch, landing
and locking. Complete the pr epar at i on s t eps listed in Chapter 3.
4
5 End Flight
Enable
Flight
Confirm that all the inspection items, including environment and the
device itself, conform to fli ght r equirements before enabling flight .
Please operate by strictly conforming to the steps described in the
chapter; the operation seq uence can't be reversed.
It is to elaborate the operation st eps after aircraft landing.
Please operate by strictly conforming to the steps described in this
II
6
Upgrade
It is to introduce upgrade methods and points of attention.
7
Appendix 1
It is to introduce the techni cal parameters.
8
Appendix 2
It is to introduce the indicator definition of the aircr aft.
9
Appendix 3
It is to introduce the matching m et hod among the components.
10 Appendix 4 It is to list possible problems and solutions when using the product.
III
Symbol Definition
Symbol
Note
ndicates a potentially hazardous situation which, if not avoided, could
No.
Versi on No.
Revision Content
Release Date
1
V1.0.0
First release
2018.02.13
The following symbol may appear in the document. Please refer to the table below for the
respective definition.
It i
result in death or serious injur y.
It indicates a moderate or low level of potential dang er w hich, if not avoided,
could result in minor or moder at e i njury.
It indicates a potential risk that, if ignored, could result in damage to device,
degraded performance, or unpr edictable results.
It means that it can help you to solve some problems or save your t ime.
It means the additional information, which is the emphasis and supplement
of the main body.
Document Material
The product includes the following document materials. Please search according to your
requirements:
Quick Start Guide
It applies to the first simple flight. Please re fer to User’s Manual for operation detai ls when it is used
for the second time or it has to use s ome other advanced functions.
Check the paper material in the packaging box or log in www.dahuasecurity.com to obtain the
User’s Manual.
User’s Manual (this document)
It comprehensively introduces the product function features, structure parameters, installation,
dismounting and flight gu i de et c .
Log in www.dahuasecurity.com to obtain the User’s Manual.
Revision Record
IV
Important Safeguards and Warnings
The following description is the correct application method of the device. Please read the
manually carefully before use, in order to prevent danger and property loss. Strictly conform to
the manual during application and keep it properly after read ing.
Please operate the aircraft in the environment which meets flight conditions, and keep
away from no-fly zone.
After unlocking, operator s shall keep at least 5m away from the aircr aft.
Please transport, use and store the product and all its components in the environment
which satisfies the require me nts.
Please strictly conform to operation flows described in the manual when dismantling the
device. Please do not dismantle other components privately.
Please do not touch the lens of PTZ camera directly. Use hair drier to remove the dust or
dirt from the lens surface.
Please operate the device by strictly conforming to the steps described in the manual; the
operation sequence can’t be rev ersed.
Get to know local laws and regulations before using the aircraft. Please apply to local
authorities for flight per mission if necessary.
For the first flight, please adopt loiter mode (before takeoff, it is suggested that GPS
satellites are ≥12 and horizontal dilution of precision ( HDOP) is ≤1).
Please make sure that the device antenna has been properly installed before enabling the
power of remote control or aircr aft. O therw ise, it may cause da mages to intern al modu le or
shorten the control distanc e.
Flight Environment
Please make flight in the env ironment which meets the followin g c onditions:
V
Keep away from no-fly z one; ple as e do not enter no-fly zone.
Keep view wide open; make sure the device is flying within field of view; please do not
block field of view.
Please do not fly the aircraft in rain, snow and thunder weather.
Please do not fly in narrow and small space.
Try not to fly r ight above the crowd, in order to prevent per sonal injury.
Please do not get close to high-voltage power line. Keep more than 10m distance.
Power Requirement
The product shall use electric wires (power wires) recommended by this area, which shall
be used within its rated specifi cat ion!
Products with category I structure shall be connected to grid power output socket, which is
equipped with protectiv e gr ounding.
Please conform to local elec t r ica l safety standards strictly.
Before operation, please c heck whether power supply is correct .
Please use power supply that meets SELV (safety extra low voltage) requirements, and
supply power with rate d voltage t hat conf orms to L imited Pow er Sourc e in IEC60 950-1. For
specific power supply requirements, please refer to device l abels.
Prevent power cord from being trampl ed or pr essed , especial ly t he plug, powe r socket and
the junction extruded from t he device.
Battery Points of Attention
It has to use the exclusive power adapter provided by Dahua Technology to charge the
device. Otherwise, it may damage the battery or lead to other unpredictable
consequences.
Charge the device at a temperat ur e between 0 and 50℃.
Distinguish positive and negative poles when charging the device, to prevent short circuit.
Charge and discharge at least once every month; prohibit storing the device without
electricity.
Please do not place the device cl ose to fire source or inflammables.
Please do not charge and dischar ge the device in unattended conditions.
Please do not use undesignated battery to the device.
VI
Please do not dismantle and destroy the batt ery without per mission; w ater is not allowe d to
enter the device; man-made damages are not covered by w arr anty .
Please do not throw the bat t er y into fire or expose it to high-temperat ur e environment.
Please do not dismantle, modi fy or deform the battery.
Avoid short circuit between positive and negative contacts (please do not place the bat t er y
together with the objects such as necklace and hairpin etc. when carrying or storing the
battery).
Please replace new battery timely when it is damaged. Please contact local relevant
agency to deal with dama ged bat t er y properly, in order to prevent accidents.
Please charge the battery or discharge it to 50%～60% remaining capacity if it won 't be
used for a long time, and plac e it in a dry and cool environment.
If the battery leaks and the liquid enters eyes accidentally, please do not rub your eyes;
wash your eyes with clean water and see a doctor immediately.
It is normal that the battery heats up after it is running for a period of time, because the
discharge power is quite big.
It is normal that the battery heats up when it is being charged.
The cycle times of power bat t er y is 300 in normal application situation.
During charging of power batt ery, charging is completed when the charger displays “FULL”
and beeps continuously. Don’t take down batteries before charging is comp le t ed.
Application Environment Requirements
Please do not aim the PTZ at str ong l ight ( such as lighting, sunlight and so on).
Please transport, use and store the device within the allowed humidity and temperature
range.
Please do not let any liquid flow into the device.
Please do not block the device ventilation.
Please do not press, vibrat e or soak the device.
Please pack the device wit h or igi nal package or material with equivale nt quality.
Operation and Maintenance Re quirements
Please do not dismantle the dev ice privately.
Please do not touch sensor CCD or CMOS directly; use hair drier to remove dust or dirt
from the lens surface.
Please use soft dry cloth o r clea n soft c loth to d ip a li ttle mil d deterg ent t o clean t he device.
Please do not touch or wipe the lens surface directly.
Please use the accessor ies pr ov ided by manu factur er and it sha ll be i nstal led and rep air ed
by professional staf f s.
Please avoid laser beam radi at ion t o t he surface when using laser bea m dev ic e.
Please do not provide two or more power supply modes to the device at the same time;
otherwise, it may damage the device.
Max 1 aircraft is allowed to fly in t he same area at the same time.
VII
Please make sure that there is no occlusion above the flight.
Special Announcement
This manual is for referen ce only. Please refer to the actual product for more details.
The user’s manual, software and firmware will be regularly updated according to the
product upgrade without p r ior announcement.
The user shall undertake any losses resulting from violation of guidance in the document.
The document may include technically inaccurate contents, inconsistencies with product
functions and operations, or misprint. Final explanations of the company shall prevail.
Interface in this manual may be slightly different from actual interface. Please refer to
actual interface for details.
Other trademarks or company names mentioned in the document belong to the respective
owners.
VIII
Table of Contents
Legal Statement ......................................................................................................................................... I
Preface ....................................................................................................................................................... II
Important Safe guards and Warnings ..................................................................................................... V
1 Product Introduction ............................................................................................................................. 1
1.1 Overview ....................................................................................................................................... 1
1.2 Functional Features ...................................................................................................................... 1
2 Structure ................................................................................................................................................. 4
2.1 Aircraft ........................................................................................................................................... 4
2.1.1 Product Dimensions............................................................................................................ 4
2.1.2 Structural Component ......................................................................................................... 6
2.2 Airborne Device............................................................................................................................. 7
2.2.1 The 2 MP Visible Light PTZ Camer a .................................................................................. 8
2.2.2 Structural Compo nent of 2 MP Visible Light PTZ Camera ............................................... 10
2.3 Remote Control ............................................................................................................................ 11
2.3.1 Dimensions ........................................................................................................................ 11
2.3.2 Structural Component ....................................................................................................... 12
2.3.3 Buttons .............................................................................................................................. 16
2.3.4 Operation Interface ........................................................................................................... 18
3 Flight Prepar at ion ................................................................................................................................ 27
3.1 Unpack ........................................................................................................................................ 27
3.2 Check Remaining Power ............................................................................................................ 27
3.2.1 Aircraft ............................................................................................................................... 28
3.2.2 Remote Control ................................................................................................................. 29
3.3 Charging ...................................................................................................................................... 30
3.3.1 Aircraft Battery Charging .................................................................................................. 30
3.3.2 Remote Control Charging ................................................................................................. 31
3.4 Prepare Airborne Device ............................................................................................................. 31
3.4.1 Demount PTZ Camera ..................................................................................................... 32
3.4.2 Install PTZ Camera ........................................................................................................... 32
3.5 Prepare Aircraft ........................................................................................................................... 33
3.5.1 Unfold Arm ........................................................................................................................ 33
3.5.2 Open Antenna ................................................................................................................... 33
3.5.3 Install Aircraft Battery ....................................................................................................... 34
3.6 Prepare Remote Control ............................................................................................................. 34
3.6.1 Install Micro SD Card ........................................................................................................ 34
3.6.2 Open Antenna ................................................................................................................... 35
3.6.3 Enable Remote Control Power ......................................................................................... 35
3.6.4 Confirm Remote Control Mod e ......................................................................................... 36
3.6.5 Set Quick Operation ......................................................................................................... 36
3.7 Enable Aircraft Power ................................................................................................................. 42
3.8 Check and Debugging ................................................................................................................ 42
IX
3.8.1 Remote Control Ca libr at ion .............................................................................................. 43
3.8.2 Accelerometer Calibration ................................................................................................ 43
3.8.3 Initialization Failure ........................................................................................................... 44
3.8.4 Geomagnetic Abnormity ................................................................................................... 45
3.8.5 GPS Satellites Insufficiency .............................................................................................. 47
3.9 Install Propellers.......................................................................................................................... 47
4 Enable Flight ........................................................................................................................................ 49
4.1 Flight Mode ................................................................................................................................. 49
4.2 Manual Mode .............................................................................................................................. 50
4.2.1 Introduction to Manual Flight Flow ................................................................................... 50
4.2.2 Unlock Flight Control ........................................................................................................ 50
4.2.3 Manual Takeoff ................................................................................................................. 51
4.2.4 Manual Flight Control ....................................................................................................... 52
4.2.5 Manual RTH and Landing ................................................................................................. 53
4.2.6 Manual Locking ................................................................................................................. 54
4.3 Intelligent Mode ........................................................................................................................... 55
4.3.1 Intelligent Flight Mo de ...................................................................................................... 55
4.3.2 Intelligent Locking M ode ................................................................................................... 59
4.3.3 Intelligent Operati on.......................................................................................................... 60
4.4 Intelligent Protection Mechanism ................................................................................................ 62
4.4.1 Low Battery ....................................................................................................................... 62
4.4.2 Out of Control ................................................................................................................... 62
4.5 Remote Control Setting ............................................................................................................... 62
4.5.1 Remote Button User-defined ............................................................................................ 62
4.5.2 Flight Control Settings ...................................................................................................... 63
4.5.3 Preview Settings ............................................................................................................... 66
4.5.4 Camera Settings ............................................................................................................... 67
4.5.5 General Settings ............................................................................................................... 70
5 End Flight ............................................................................................................................................. 75
5.1 Turn off Power ............................................................................................................................. 75
5.2 Remove Aircraft Battery .............................................................................................................. 76
5.3 Dismantle Airborne Device ......................................................................................................... 77
5.4 Fold Aircraft ................................................................................................................................. 77
5.5 Copy Video of Camera Micro SD Card ....................................................................................... 79
5.6 Remove Other Component s ....................................................................................................... 79
6 Upgrade and Update......................................................................................................................... 80
6.1 Firmware Update......................................................................................................................... 80
6.2 Remote Control Update .............................................................................................................. 80
6.2.1 APP Update ...................................................................................................................... 80
6.2.2 Download and Upda t e O ffline Map of Remote Contro l .................................................... 81
Main Techni cal Parameters ............................................................................................. 82
Aircraft State Indicator ................................................................................................... 85
System Pairing .................................................................................................................. 87
FAQ .................................................................................................................................... 89
Appendix 4.1 FAQ and Solutio ns of Aircraft ..................................................................................... 89
Appendix 4.2 FAQ and Solutio ns of Remote Control ....................................................................... 89
Appendix 4.3 FAQ and Solutio ns of Airborne Device ....................................................................... 89
X
Appendix 4.4 FAQ and Solutions of Charger .................................................................................... 89
XI
1.1 Overview
This product is a hex-rotor drone d esi gned f or pub lic security, transportation, firefighting, border
defense, agriculture, forest and energy source fields. It provides integrated solutions of aerial
video surveillance.
This product consists of air cr aft, airborne device and remote control.
Aircraft: It consists of navi gat ion system, flight control system a nd power system.
Airborne device: It consists of the PTZ control system and mission device.
Remote control: It consists of the remote control system, data chain and software.
1 Product Introduction
1.2 Functional Feat ures
Integrated Design
The aircraft adopts integrated design and neat appearance. Only the propeller shall be
dismantled and installed.
The remote control integrates the remote control and touch screen together. It is easy to
operate and has clear indicator.
Folded Packages
Arm can be folded repeatedly.
Antennas can be folded repeat edly, suitable to be carried, transported and stored.
Quick Dismantling
The propeller adopts quick dismantling structure.
It is easy to open or fold arm and antenna.
The PTZ camera adopts quick dismantling structure. Installation screws are secured on
the shock absorber plate, in order t o pr event them from being lost.
HD Video
The shock absorber board and shock absorber ball work together to guarantee PTZ
Industrial 30x optical zoom visible light camera is optional, with professional HD video
camera stability.
1
effect.
IR thermal camera is opt ional, su itab le for sp eci al en v ironments su ch as fire s cene or night
environment, so as to guar ant ee clear video and high restoration t hermal images.
The remote control has snapshot button and record button, which are easy to operate and
instantly start snapshot an d r ecor d f unc tion.
Accurate Positioning
Built-in GSP system ensures that positioning is accurate and real-time.
Wireless Transmission
Aircraft has 4 antennas. Connect the remote control and image transmission device to
send and receive radio wave signals.
The remote control has 3 antennas. Connect the aircraft to send and receive radio wave
signals.
Low Electric Quantity Protection
When electric quantity is lower than estimated safe return value, trigger low electric quantity
protection automatically, including alarm, return home and landing.
Intelligent Battery
Display remaining electr ic quantity: Battery has built-in power i ndicator light.
Balanced charging protection function: Automatically balance the battery cell voltage to
protect battery.
Overcharge protection function: Battery automatically stops charging when the voltage is
full.
Sleep protection function: Battery automatically goes to sleep state when there is no
operation within 5 minutes .
Charging temperature pro t ection fun ction: Th e batt er y c harging te mperat ure r ange s from 0 ℃
to 50℃. Once the temperature is too high, bat ter y automat ical ly st ops chargin g; other wise,
it may result in battery damage.
Communication: The r emote control can get remaining capacity and voltage information.
Flight Control
The aircraft adopts hex-rotor power system. It can switch among several flight modes and
control the flight direction flexibly.
Support 14,500g maximu m take-off weight.
Support binocular obstacl e avoidance, optical flow positioning, R TK and protection in case
of broken propeller.
Electronic Fence (e-fence)
Support e-fence functio n; pr event the aircraft from leaving the specified flight zone.
2
Support customized e-f ence settings.
3
2 Structure
This product mainly consists of aircraft, airborne device and remote control. This chapter
introduces the structures of these 3 components. The detailed operations will be introduced in
“3 Flight Preparation”.
All figures listed below and all dimensions listed here for reference only. The figure and the
dimensions may be slightly different from the user data due to measurement position,
measurement accuracy and position indication. Please refer to the actual product for detailed
information.
2.1 Aircraft
This section is introduced when the propeller is installed completely and the whole device is
unfolded. Please refer to Cha pt er 3 for details.
2.1.1 Product Dimensions
Unit is mm.
Figure 2-1
4
Figure 2-2
5
2.1.2 Structural Component
No.
Name
Function
according to the actual sit uat ion.
2
Arm
Fold and unfold.
Protective cover of
After the battery is installed into the aircraft, battery buckle
shall be closed!
1 Propeller
3
4 Battery buckle
propeller
Figure 2-3
High-speed revolution to turn the brushless motor power to
propulsive force.
There are 3 pairs of propellers (3 CW propellers and 3 CCW
propellers) with different structures. Please install propellers
Fix the horizontally unfolded arm.
Dismantle and install the battery.
When it is opened, battery can be dismantled from the
device and replaced.
When it i s c l ose d , the battery cannot be dismantled from
the device.
6
No.
Name
Function
switch (with
Built-in indicator.
middle part indicates aircraft tail.
Motor speed
controller
With sine wave driving, have excellent acceleration and
deceleration performance.
Control the landing gear to open or fold with remote control
There are two modes: normally on and flashing. It displays
five colors: red, yellow, blue, green and purple, to indicate
er to Appendix 2 for indicator light information and
definition.
Heat dissipation
Built-in binocular heat dissipation module (cooli ng f in).
This module has different structures depending on device
configurations. Pleas e refer to actual product.
5
Power
indicator)
After the aircraft is power on, red indicates power-on state,
while green indicates re m ain ing battery.
6 Empennage Built-in GPS and elect r onic compass.
Fold or unfold.
7 Antenna
2 antennas are to receive the r em ot e cont r ol signal.
2 antennas are for wireless image transmission.
Display red and green.
Two adjacent indicators are normally on in red; their
middle part indicates aircraft nose.
Four adjacent indicators are normally on in green; their
8
Motor control panel
indicator
9 Motor Drive propeller rotation.
10
11 Landing gear
buttons.
12 Aircraft state indicator
13
module (cooling fin)
2.2 Airborne Devic e
system state, flight mode, upgrade state and et c.
Ref
Table 2-1
This part takes visible light PTZ camera and IR thermal PTZ camera as an example, and
introduces airborne devic e.
For detailed info about various airborne device, please refer to their user’s manual s and
quick start guides.
The aircraft supports to carry 2 MP visible light PTZ camera and multiple airborne devices.
7
2.2.1 The 2 MP Visible Light PTZ Camera
Unit is mm.
Figure 2-4
8
Figure 2-5
9
No.
Name
Function
1
Shock absorber ball
Reduce PTZ camera vibration during the flight, to get
2
Shock absorber board
3
Installation screw
Secure the PTZ camera on t he aircr aft.
4
Course motor
2.2.2 Structural Component of 2 MP Visible Light PTZ Camera
Figure 2-6
clearer video.
Control horizontal directi on of the camera.
5 Course rotation arm
6 Roll motor
Control horizontal inclination angle of the camera.
7 Roll rotation arm
8 Pitching motor Control vertical pitching angle of the camera.
9 Camera
Take pictures.
10 Lens
Table 2-2
10
2.3 Remote Control
2.3.1 Dimensions
Unit is mm.
Figure 2-7
11
2.3.2 Structural Component
Front panel, side panel and rear panel of the remote control are shown in Figure 2-9, Figure
2-10 and Figure 2-11.
Figure 2-8
12
No.
Name
Function
while two yellow antennas are installed at both sides.
2
Hanger
Fix the hanger belt.
Left control
Landing gear
connecting power to the charging
click return
button
Figure 2-9
Establish the remote control relationship with the aircraft and
1 Antenna
3
joystick
receive images. One silver antenna is installed in the middle,
Control the aircraft flight state.
4 Touch screen Set parameters and preview the video.
5
button
Control the landing gear.
6 Battery indicator Each bar represents 25% bat t er y power.
Indicator light is on when
7 Charging indicator
8
One-
port.
Red light is normally on: chargi ng.
Green light is normally on: charging is finished.
Control aircraft to return h om e aut omatically.
9
One-click
takeoff/landing
button
Control aircraft takeoff or landing with one click. Takeoff height
is 2m.
13
No.
Name
Function
Right control
No.
Name
Function
Upper level: intelligent flight mode. The aircraft flights
are at the central mode, the aircraft hovers at the same
Reset button of
PC.
10
joystick
Control the aircraft flight state.
Table 2-3
Figure 2-10
11
PTZ course scroll
wheel
Control horizontal shooti ng angle of camera lens.
12 Snapshot Press this button shortly to snapshot present image.
3-level lever to select flight mode.
automatically accordin g t o the specified course.
Middle level: flight at the specified height. When the throttle
13 Flight mode lever
lever is at the central mode, the aircraft flights at the same
height automatically.
Lower level: flight at the specified position. When all levers
position.
14 4G SIM slot Support 4G function.
15 Audio output port Connect to earphone, sou nd box and etc. It is to play audio.
16
remote control
17 Micro USB port
Reserved.
Insert data cable to connect PC. It is to transmit the data to the
14
No.
Name
Function
18 SD slot
Insert micro SD card: The micro SD card with the chip is
micro SD card pops up a little bit, and can be pulled out.
19
Power port
Input DC 12V power.
2-level lever. It is to select PTZ mode.
Lower level: Course locking mode. No matter what the
same degree to shoot.
Press this button shortly to start recording, and press it again to
PTZ pitch scroll
No.
Name
Function
Press it for a short time, to zoom in the camera.
the maximum magnification.
24
Power switch
Turn on or tur n off the remote control.
20 PTZ mode lever
facing down. Insert the ca r d t o t he slot hor iz ontally.
Remove micro SD card: Press micro SD card inwards, so
Upper level: Course follow ing mode. The PT Z ca mera angl e
changes with aircraft flight direction.
aircraft flight angles are, the PTZ camera always faces the
21 Record button
22
wheel
stop recording.
Control vertical shooting a ngle of camera lens.
Table 2-4
Figure 2-11
23 Zoom in button
Press it for a long time, to zoom in until the camera reaches
15
No.
Name
Function
25 Zoom out button
Press it for a short time, to zoom out the camera.
Press it for a long time, to zoom out until the camera
2.3.3 Buttons
Refer to Chapter 4 for the joystick and flight mode lever butt on infor m at io n.
2.3.3.1 Scroll Wheel
reaches the minimum magnification.
Table 2-5
Besides “PTZ Course Scroll Wheel” and “PTZ Pitching Scroll Wheel” of remote control, control
PTZ “PZT Center” and “PTZ 90°” through “State Bar > Quick Operation > PTZ”. Please refer to
“3.6.5.2 PTZ” for details.
PTZ course scroll wheel: control horizontal shooting angle of camera lens, as shown in
Figure 2-12.
Scroll wheel turns to the left: PT Z t ur ns t o the left.
Scroll wheel turns to the right: PTZ turns to the right.
Figure 2-12
PTZ pitching scroll wheel: control vertical shooting angle of camera lens, as shown in
Figure 2-13.
Scroll wheel turns to the left: camera lens turns downwards.
Scroll wheel turns to the right: camera lens turns upwards.
Figure 2-13
16
2.3.3.2 PTZ Mode Lever
Shooting direction of PTZ camera is controlled with PTZ mod e lever, as shown in Figure 2-14.
2-level lever:
Upper level: Course following mode. Shooting angle of PTZ camera changes with aircraft
flight direction.
Lower l evel: Course locking mode. No matter what the aircraft flight angles are, the PTZ
camera always faces the same degree to shoot.
Lever returns to the center: start from any position, move the lever for three times
continuously. Shooting angle o f P TZ camera will be consistent with a ircr aft flight direction.
2.3.3.3 Shooting
Figure 2-14
Figure 2-15
17
Snapshot: Press snapshot button for a short time to snapshot t he pr esent image.
No.
Name
Function
Function setting
list, flight mode, remote control signal intensity, GPS signal
Quickly switch video preview and map preview to display
Display remaining flight time, aircraft speed, height and
Bar” for details.
Record: Press record button for a short time to begin recording video. Press it for a short
time again to stop recording.
2.3.4 Operation Interface
After turning on with the remote control, enter main interface. It consists of the following
function modules, as sho w n in Figure 2-16.
Figure 2-16
Slide up at any positio n on the prev iew inter face to h ide the s etting m enu, funct ion bar and state
bar. Slide down at any position on the main inter f ace to view them again.
Set the menu and aircraft course; d isplay PTZ mode, flight state
1
and state bar
intensity, image transmission signal quality, aircraft battery and
quick viewing.
Please refer to “4.5 Remote Control Setting” for spec i fi c set ti ng
items and descriptions.
2 Preview window
prompt information and PTZ control. Please refer to “2.3.4.3
Preview” for details.
3 State bar
distance from the HOME. Please refer to “2.3.4.2 State Display
Table 2-6
18
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