AP10.1 autopilot is designed to control the vehicles automatically, semi-automatically or manual modes.

The system is configurable for the following platforms:

• for the airplanes take-off from the runway and landing on the runway in automatic mode
• for the helicopters take-off and landing in automatic mode
• for boats
• for lighter than-air aircraft

AP10.1 can be installed on aircraft with weight over 100 kg (for the lighter aircraft we recommend Mini version – AP10.2, or Micro version – AP10.3).

Main benefits:

• extended modular configuration
• system out-of-the-box insulation against vibrations

Payload of almost any type can be connected and controlled using the interfaces:

• 1-Wire
• RS-232
• RS-485
• UART
• CAN

• control of actuating mechanisms
• engine control
• semi-automatic control with automatic stabilization of the vehicles
• manual control using the main 928MHz communication channel
• from ground control station (GCU)
• control of the vehicles object in emergency mode
• payload control
• payload feedback
• control of rotating platforms in gyro-stabilization mode using AP10.1
• receipt and transfer of telemetric data between GCU and the vehicles
• simulation mode
• flight simulator
• onboard power control
• power stabilization
• conversion
• power distribution, including emergency power supply mode
• onboard power monitoring

Available Interfaces:

• up to 15 x servo drives (PWM control)
• 2x inputs for RPM sensor (Hall-effect sensors)
• 1-Wire interface
• TTL UART interface
• RS-485 interface
• Controller area network - CAN
• RS-232 interface
• Low-side power output (3.7A, @ 20V, 68MOhm)
• 3x digital inputs (timing, level)
• 5x general purpose inputs-outputs (remappable on MCU)

Technical specifications:

Operating temperature	IP rating	Housing material	Connector
-40°C to +60°C	IP67	Aluminium alloy	Amphenol PT02E12-10P Amphenol PT02E8-4P Amphenol PT02E18-32P SMA

Power supply	Protection
7-27 V	All digital logic inputs and outputs are protected	ESD protection	Power supply reverse-polarity protection

 

AP10.1 system configuration for airplanes example:

#	Item	Designation	Part number	Weight, g
1	AP10.1 Kit
1.1	Onboard Telemetry Unit	OTU	UV01.431329.100.310	170
1.2	Interfaces Controller	IFC	UV01.431329.100.332	100
1.3	Onboard Antenna	OA	UV01.431329.100.315	300
1.4	GPS Receiver	GPS	UV01.431329.100.346	67
1.5	Central Processing Unit	CPU	UV01.431329.102.330.00	160
1.6	Pitot Tube	PT	UV01.468339.80.341	62
1.7	Data Processing Unit of Pitot Tube	DPU-PT	UV01.431329.100.320	230
1.8	CAN-HUB	CAN-HUB	UV01.468353.01
1.9	Angle of Sideslip Transmitter	AST	UV01.431329.05	180
1.10	Power distribution, switch unit	PSU	UV01.431329.07
1.11	Flight recorder	FR	UV01.431329.11
1.12	Emergency rescue system controller	ERSC	UV01.431329.06
1.13	Onboard antenna	OA	UV01.431329.100.315
2	Optional airborne equipment
2.1	Antivibration mounting for CPU (for UAVs MTOW more than 200 kg)		UV.431329.90.330-10.00	4600
2.2	Laser Altimeter (0-100 m altitude)
2.3	Radio Altimeter (0.3-400 m altitude)
All housings are hermetic.
3	Ground control unit
3.1	GCU  ground telemetry unit	GCU-GTU	UV01.431329.100.211	110
3.2	GCU  antenna	GCU-A	UV01.431329.80.215	400
3.3	Portable ground control station *	PGCS	UV01.468323.01	19500

* Exploitation of Uavos PGCS is optional. Required software (GCU) can be installed on any computer under Linux OS control