JTT T60C User manual

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CONTENT
1. SYSTEM COMPOSITION AND ASSEMBLY.............................. - 6 -
1.1. SYSTEM CONFIGURATION LIST .......................................................................- 6-
1.2. ASSEMBLY AND CONNECTION OF AIRCRAFT...............................................- 7-
1.3. OPERATION AND THE USE OF CHARGER ......................................................- 9-
1.4 .DESCRIPTION AND USE OF THE REMOTE CONTROL ............................. - 12 -
2. AIRCRAFT..................................................................................................... - 15 -
2.1. AIRCRAFT MODE.................................................................................................. - 15 -
2.2. STATUS INDICATOR OF AIRCRAFT ............................................................... - 17 -
3. GROUND CONTROL STATION....................................................... - 18 -
3.1.COMPOSITION OF GROUND CONTROL SYSTEM ....................................... - 18 -
3.2. OPERATIONS OF GROUND CONTROL STATION....................................... - 23 -
3.3. SOFTWARE OPERATION.................................................................................... - 27 -
3.3.1. Connection .............................................................................................- 27 -
3.3.2. Main interface ......................................................................................- 28 -
3.3.3. Quick Access Toolbar ...................................................................- 31 -
3.3.4. Arm/DisArm ...........................................................................................- 35 -
3.3.5. take-off .......................................................................................................- 36 -
3.3.6. Real-time aircraft guide ................................................................- 36 -
3.3.7. Guided flight ..........................................................................................- 37 -
3.3.8. GUIDED cruise ...................................................................................- 38 -
3.3.9. Automatic Cruise ...............................................................................- 41 -
3.3.10. Interest Point .....................................................................................- 50 -
3.3.11. LANDING ..............................................................................................- 51 -
3.3.12. RTL ............................................................................................................- 52 -
3.3.13. HOVERING .........................................................................................- 52 -
3.3.14. ALTHOLD .............................................................................................- 53 -
3.3.15. Change the height and speed .............................................- 53 -
3.3.16. Real-time status data ..................................................................- 54 -

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3.3.17.fault protection ...................................................................................- 55 -
3.3.18 Geographical rail ..............................................................................- 56 -
4. INSTRUCTIONS FOR FLYING.......................................................... - 57 -
4.1. CHECK UP BEFORE FLYING.............................................................................. - 57 -
4.2. AIRCRAFT CALIBRATION .................................................................................. - 57 -
4.3. ANALYSIS AND ANSWERS TO FAQ.............................................................. - 60 -
4.4. WARRANTY INFORMATION ............................................................................. - 60 -

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Danger
Subject to Special Controls, and any wrong operation may result in damage to the
goods, personal injury or even casualty. For any such accident, the user shall bear the
corresponding criminal responsibility. It isn’t recommended that the product is used by
juveniles less than 18 years old. To make better use of this equipment and to ensure
your safety, before you use it, please carefully read the user manual, or to consult with
the after-sales or customer service personnel. You can directly log on the company's
official website (http://www.jttuav.com/) for product-related information.
Warnings
●please keep the electrical parts out of reach of the children;
●to ensure that the aircrafts are away from the crowd and dangerous goods during
●It is recommended that the aircraft flies in a special flight site;
●Do not operate the aircraft when you are tipsy, fatigue, or in poor mental state.
●please operate in strict compliance with the user manual.
●before cruise, make sure that the power supply system and other functional modules
are correctly connected, or else it will result in the overturning of equipment.
●before you perform channel calibration, firmware update and parameter setting for
the remote, please switch off the power supply or remove the airscrew to prevent the
sudden high-speed revolution of motor.
●it is forbidden to fly in severe environment.
●don’t turn on the aircraft system, or modify the equipment structure without
permission. You need to be responsible for any possible consequences thereby.
●Please don't impact, break off or squeeze the electrical stand, and make sure that the
taking off and landing site is flat, or else it may affect the service life of electrical stand.

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Disclaimer
1.The products are subject to the Special Controls, and the user will be fully
responsible for the use of this product. The manufacturer does not assume any
responsibility for any consequences caused by direct or indirect use of these products.
2.During the use of this product, the user shall be liable for any violation of public order
or public safety.
3.We do not provide any technical support and security commitments under the
following situations:
（1）The unit or individual who obtains the products through non-normal agent or non-
normal channels.
（2）Products with unauthorized modification, commissioning and replacement of
parts.
（3）The products without warranty card, serial number or flight data. Caused by
personal operation error or natural disasters

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1. SYSTEM COMPOSITION AND ASSEMBLY
1.1.System Configuration List
Serial No.
List
1.
T60 airframe *1
T60 arm *6
T60 airframe (including flight control
system, image transmission system, digital
transmission system and electronic system).
T60 arm （including motor, electronic
speed controller and paddle）
2.
T60 stand*2
ground control station *1
3.
remote *1
power battery *3

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4.
image transmission antenna *1
data transmission antenna *2
5.
antenna extension cord *2
metal image transmission antenna *2
1.2.Assembly and connection of aircraft
Step 1: open the packaging aluminum case of aircraft and take out the relevant
components of aircraft for further installation.
Step 2: take out two "T-shape stands" from the aircraft parts, and mount them on the
casing of aircraft, and tighten the rotary knob of stand. The specific operation is shown
in Figure 1.2.1 below.

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（Figure 1.2.1）
Step 3: connect six arms of aircraft correspondingly according to the number and
tighten them clockwise. The specific operation is shown in Figure 1.2.2.
（Figure 1.2.2）
Step 4: have the supportive data transmission/image transmission antenna of aircraft
installed according to the corresponding locations;
Step 5: instructions for installation of payload equipment
Take out the payloads from the packing case, and quickly install it to the drone, tighten
the quick release device. Connect power line and control line accordingly as shown in
Figure 12.3.

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（Figure 1.2.3）
1.3.Operation and the use of charger
The aircraft is charged following the steps below:
Step 1: take out the power battery of ground control station/UAV (unmanned aerial
vehicle).
Step 2: after you have completed the wiring as follows, the power supply unit is
connected to the AC at 220V, and then the aircraft can be powered on by turning on
the rocker switch. Details are shown in Figure 1.3.1.

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（Figure 1.3.1）
Step 3: after the charging circuit is correctly connected, first press the STOP/START 1
or STOP/START 2 button and rotate the round button in the middle. Select the battery
option of “0 LiPo” and confirm the setting by pressing the round button in the middle,
as shown in Figure 1.3.2.
（Figure 1.3.2）
Stop or
start
button
Round
button

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Step 4: rotate the round button in the middle and put the cursor on “Charge” and then
press “TAB/SYS” to perform data setting on the right side. Set the “LiPo Cap”as
“Ignore”, and “Cells” as “22.2V 6S”, and “Current” as “15A”, and “Chg Mode” as
“Normal Balance”.
（Figure 1.3.3）
Step 5: rotate the cursor to "Start", and click rotary switch to confirm, and you just need
to select "YES" to charge the lithium battery, as shown in Figure 1.3.2.
（Figure 1.3.4）
The
charging is
confirmed.
Char
ging
curre
nt

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Step 6: when the lithium battery is fully charged, click on "STOP/START 1 or
STOP/START 2" button, and then turn the middle button to "Charge", press the middle
button to enter to the interface and adjust the battery voltage. The voltage of single
battery is about 4.2V, and the total voltage is 25.2V. The battery is disconnected after
being fully charged, and you just need to disconnect the power supply, as shown in
Figure 1.3.2.
（Figure 1.3.5）
1.4 .Description and use of the remote control
Serial no.
Name of
switch
Function Description
1
LDrotary switch
to control the tilting of cradle head of high-definition camera
2
3
SB and SA three-gear
switch
Gear
SA
Gear
SB
Operating mode
Gear
1
X, that is,
any stability
Augmentation.
Manual mode is of the highest
priority. In any mode,
if SA switch turns back to the Gear
1,
and the flight mode is manual
stability augmentation.
Gear
3
Gear 1
AUTO GPS

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Gear
3
Gear 2
AUTO navigation
Gear
3
Gear 3
RTL LAND
4
Left rocker
Throttle (upward and downward)/course rocker (left and right)
5
Power switch
Slide upward to turn on while slide downward to turn off.
6
Remote Control display
menu display
7
antenna
Ground receiving antenna
8
RDrotary switch
controls the heading of cradle head of high-definition camera
9
SC three-gear switch
Gear 1 of SC controls the LD switch of control cradle head's
tilting (adjustable).
Gear 2 of SC, controls the tilting of cradle head and the rolls of
LD and RD switch (adjustable).
Gear 3 of SC, controls the LD and RD switches of tapered end
mode of control cradle head.
Switch Gear SC to Gear 1, and the cradle head returns to the
middle in the follow-up mode, and the tilting LD switch
(adjustable).
10
SD three-gear switch
Prod upwards (put the stand down), and prod downward (the
stand rises).
11
Right rocker
tilting(upward and downward)/(left and right)rocker
12
touch key of
function menu
Remote controls of menu buttons of all functional channels
The specific numbering is indicated by Figure 1.4.1 below

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（Figure 1.4.1）
Instructions for remote:
(1) The handset is switched on: every time before the task the implemented, turn on
the remote first and then turn on the aircraft. Every time the flying task is completed,
turn off the aircraft and then power off the remote (In case the accidents occur.)
(2) The battery capacity of remote: the normal voltage of remote is 5.8V-7.2V; every
time you implement the flying task; make sure that the battery capacity of remote is
sufficient. In case of low battery, charge the remote battery in time.
(3) Arm flight: when the aircraft and the ground control station are normally powered on,
the aircraft is connected through the ground control station, and the ground control
station obtains the real-time data of aircraft. If parameter is normal , and HDOP value
≤1, it can be unlocked by operating the rocker to “╮╭”on the remote.
Note: The take-off point of UAV (unmanned aerial vehicle shall be set in the open and
uncrowned site. During the flying, the operation range shall not be too great. Don't prod
other switch gears without permission during flying.
choose Yes. (Notice, you could also to SE mode)

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2. aircraft
2.1. Aircraft mode
Main modes contain Manual mode, ALTHOLD mode, GPS mode, RTL mode, LAND
mode, AUTO mode and GUIDED mode.
Manual mode: the control is flexible, and the stance and height are controlled by the
operator. This is better performed by experienced user.
ALTHOLD mode: in this mode, the flight height is controlled with throttle. The current
height is locked at the Throttle position of 40%~60%. In the state, the flight height is
automated determined. The user just needs to focus on the tilting, Roll and course at
the vertical direction. This operation is simple.
GPS mode: in this mode, the Throttle controls the flight height, and the current height is
locked at the Throttle positions of 40%~60%. The aircraft is fixed based on the GPS
signal. After the user operates the rocker to return it to the middle, the aircraft remains
the same position at the horizontal direction, and the height is kept in the vertical
directions.
RTL mode: the RTL and LAND state can be realized only with reliable GPS signal.
When the current height of aircraft is lower than 15 meters, the aircraft will make a
return voyage and land on the take-off point after automatic ascending for 15 meters; if
the current height of aircraft is higher than 15 meters, the aircraft will remain at the
current height and make a return voyage.
LAND mode: When the mode is triggered, the aircraft will be landed right here
according to the current position.
Note:
1. In the GPS mode, make sure that the GPS signal is successfully located and locked
before the aircraft is unlocked, or else, the unlocking is impossible in this mode. In the
flying process, make sure that the GPS signal is successfully located and locked, or
else, it is impossible to switch to the GPS mode.
2. If any phenomenon such as weak, abnormal, interrupted or fault GPS signal and so
on appeared in the GPS mode during the flying process, please switch to the STAB
mode timely.
3. In GPS mode, the automatic switch will be performed according to the current GPS
signal; if the GPS signal is poor, the flight control will automatically switch to

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determined height; if the barometer is abnormal, the mode will automatically switch to
manual mode.
AUTO mode: the AUTO mode is the autonomous task realized based on the GPS
mode, with autonomous navigation and AUTO flying operation. In the air route mode,
the settings such as GUIDED planning, GUIDED actions and flying parameters and so
on shall be made by combining the ground control station software’s. There are two
ways of settings based on the GUIDED, one is to set the air route by means of task,
and the other one is to set the air route by means of real-time command.
In this mode, the task mode is adopted to set the air route. Before the aircraft is
unlocked, write the planned air route, flight actions and flying parameters to the flying
Controller through the ground control station, and such air route setting is called as
task mode. The aircraft will cruise according to the preset course and actions. After the
mode is triggered, the aircraft will automatically take off, plan air route and land and so
on, to complete the entire flight course task.
Note: in the mode, after the air route is successfully set, there is no need to connect
the aircraft through the ground control station, and the aircraft will cruise based on the
set air route. In this mode, the unplanned modification of flight course task. In the case
of any abnormal phenomenon in the flying process, it can be switched to the STAB
mode.
GUIDED mode: in the mode, the instruction mode is adopted to set the air route for
real time guide. After the flying is unlocked, or in the flying process, the ground control
station may set the air route in an unplanned style in this way. In this state, what the
flying controller receives is the real-time command. When the current GUIDED actions
are completed, the ground control station will send the information of next GUIDED to
the flying Controller. This method is quite flexible.
Note: the air route setting in the mode requires real-time receiving of instructions from
ground control station. The reliable real-time communication between the ground
control station and the aircraft shall be maintained, or else, the aircraft can't correctly
respond to the commands for the air route setting. If the aircraft doesn't receive the
instruction of next GUIDED, it will maintain the GPS at current positions. If any

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abnormal phenomenon occurs in the flying process, it can be switched to the STAB
mode.
2.2. Status indicator of aircraft
2.2.1 LEDindication status and significance
Conventional
functions
Initialization
Red, green and blue are
flashing alternately
out of
control state
yellow indicator
constantly glows
warning of low
battery
The yellow indicator flashes fast
(twice one second)
extremely low
battery
The red indicator flashes fast
(twice one second)
uneven
placing(unlocked)
The purple indicator flashes slowly
(once two second)
fatal error
red indicator
constantly glows
The data of magnetometer is incorrect,
which needs calibration.
The red and yellow indicators flash
fast
alternatively (twice one second).
GPS unlocked(unlocked)
The blue indicator constantly
glows
GPS locked(unlocked)
The green indicator constantly
glows
GPS mode, air route mode, unlocked
(unlocked)
The green indicator constantly
glows
GPS mode, air route mode, locked
(Armed)
The green indicator flashes
slowly (once two seconds)
STAB mode Armed）
The blue indicator flashes slowly
(once two seconds)
RTL mode Armed）
The purple indicator flashes slowly
(once two second)
Calibrate the electronic speed controller
or obtain the modified value.
The red, green and yellow indicators
flash consecutively.
Calibration
state
Enter the
calibration
stage
Ready to enter the
calibration mode
of remote
Red, blue and green indicators
change alternatively
The
remote
calibrates
the
magnetomete
r
Enter the calibration
prompt (the five
channels switch for
5~10 times, with the
intervals
of 0.8 seconds).
The blue indicator glows constantly,
which lasts for 3 seconds.
The current calibration
is completed.
The green indicator glows for 1
second
and then goes out.

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When the previous one
is calibrated or
incorrect.
The red indicator glows for 1 second
and then goes out.
Two sides are
calibrated.
The green indicator flashes twice
every
second, which lasts for 5 seconds.
The calibration of two
sides fails.
The red indicator flashes for twice
every second, which lasts for 5
seconds.
calibration
and
horizontal
calibration
Enter the calibration
prompt (the five
channels switch for
20~25 times, with the
intervals of 0.8
seconds).
The green indicator glows
constantly,
which lasts for 3 seconds.
The calibration is
successful.
The green indicator flashes twice
every second, which lasts for 5
seconds.
The calibration fails.
The red indicator flashes twice
every second, which lasts for 5
seconds.
Calibration
electronic
Speed
controller
Enter the calibration
mode of electronic
speed controller twice.
The red, green and yellow indicators
flash consecutively (flashes fast).
Note: when flying in the external field, it is suggested that it takes off when HDOP ≤1.
3. Ground control station
3.1.Composition of ground control system
The control system of ground control station is composed of ground control station,
image transmission receiving antenna and data transmission receiving antenna.

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The schematic diagram of interface positions of ground control station is shown as
（Figure 3.1.1）
(1)Instructions for image commissioning
The instructions for the function button of 15.6-inch HD LCD PANEL of ground control
station are as follows, with schematic diagram as per Figure 3.1.2.
a.SOURCE: the key is designed to provide options of the video signal source, and the
signal source has two options, that is, power supply and HDMI, respectively. The video
input source here is HDMI, and then the transmitted image can be displayed.
b."MENU / ◄”: the function is "menu / return to the next level"; in the standby mode,
click "MENU / ◄" button and it will pop up the menu option, and you can enter the
menu to set parameters. After entering the detailed project conditions, "MENU / ◄"
enables the return to the previous level.
c."▼": the function of it is to make "cursor moves downward". In the menu interface, the
cursor can be moved downward for one time in a circulating style, and you can move it
to the desired option to determine the required operation.
d."►”: the key is for "OK / enter". During the commissioning process, through the
"LEFT", you can move the cursor to the desired function, and press the "►", and you
can enter settings and make confirmation.
e."EXIT": the button is used to "exit". During the commissioning process, you can press
the "EXIT" button to exit commissioning in any status.

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f."ON / OFF" key: the key is designed for "on / off" screen operation. Just press the
"ON / OFF" button, you can turn on the 15.6-inch HD LCD PANEL (green indicator
lights, which indicates that the display is already turned on), or Press the "ON / OFF" to
turn off the 15.6-inch HD LCD PANEL (green indicator goes out, which indicated that
the display has been turned off).
（Figure 3.1.2）
(2)Power module
The power module of ground control station is composed of power supply part and
charging part.
The power supply part is powered by the lithium battery of 20000mAh. You just need to
connect the female of lithium battery XH-6P, and the positive pole (red line) and
negative electrode (black line) of lithium battery to the male, red line and black line of
XH-6P inside the ground control station correspondingly, the ground control station can
be started with one button through the metal switch on the panel.
The interface of charging part is composed of XH2.54mm 6P socket and XT 60 plug,
and the lithium battery inside the ground control station can be charged through the
charging interface on the panel, or it can be charged through the adapter by removing
the lithium battery.
Note: it is suggested that, when the ground control station isn't used, take out the
battery and store it in the battery box, and keep it in low-voltage state. Make sure that
the battery is fully charged before use.