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AP10.3 - Automatic control system for UAV (Micro version)

Current hardware version: AP10.3 - 468339.103.000 Specification (PDF)
Autopilot software documentation


AP10.3 system purpose is to control moving objects automatically, semi-automatically or manually.
At the moment we have developed the system configurations for the following unnamed systems:

- fixed-wing aircraft
- rotary-wing aircraft

AP10.3 is being used for installation on aircrafts up to 15 kg, it has such benefits:
- reduced weight and dimensions (avionics - less then 130 g)
- reduced energy consumption
- IP rating IP67

Almost any payload type can be connected and controlled through the interfaces:
- 1-Wire
- RS-232
- RS-485

AP10.3 system configuration for atmospheric satellite:

Autopilot configuration example for helicopter UAV  

Basic modules of AP10.3 system

Data Processing and Navigation Unit
Data Processing Unit of Pitot Tube Micro GPS receiver mini Pitot Tube Micro


Main functions of the AP10.3 (automatic control system of moving objects):

-automatic control of a moving object
- operating mechanisms control
- engine control
- semi-automatic control with automatic stabilization of a moving object
- manual control via the main 928MHz communication channel
- from ground control station
- control of a moving object in emergency mode
- payload control
- payload feedback
- rotating platforms control in gyro stabilization mode
- telemetrics receipt and transfer between control GCU and a moving object
- ground simulation mode – flight simulator
- operator training in flight simulator with a/c virtual model downloaded
- pre-flight a/c and flight assignment testing
- onboard power control
- power stabilization
- conversion
- distribution, including emergency power supply mode
- onboard power monitoring


Technical specifications:

Operating temperature IP rating Housing material Connector
-40°C to +60°C IP67 aluminum alloy Harwin M300-3240696M1
Amphenol PT02E14-19P
Amphenol PT02E8-4P
Harwin M80-9420605
Power supply Protection
5-27 V Gated logic on all digital IO pins ESD protection Power supply reverse-polarity protection


System Application Cases

Fixed-wing aircraft Atmospheric satellite Quadrocopter
Fixed-wing Atmospheric satellite Quadrocopter


AP10.3 System package configuration:

# Description Designation Part number Weight, g
 1 Automatic control system equipment list
 1.1 Data Processing and Navigation Unit  DPNU  UV01.468339.102.332  52
 1.2. GPS receiver mini  GPS-M  UV01.431329.102.365  49
 1.3 Pitot Tube Micro  PTMicro  UV01.468339.103.346  10
 1.4 Data Processing Unit of Pitot Tube Micro  DPU-PTM  UV01.431329.103.320  18
 All housings are hermetic.
 3 Ground control unit   
 3.1 GCU  ground telemetry unit  GCU-GTU  UV.431329.90.211  110
 3.2 GCU  antenna  GCU-A  UV.431329.80.215  400
 3.3 Extended portable ground control station *  EPGCS  UV.468323.01  28000

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