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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

Application

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
- TTL UART
- CAN

AP10.3 system configuration for atmospheric satellite:

Autopilot configuration example for helicopter UAV  

Basic modules of AP10.3 system

Data Processing and Navigation Unit
bcpm-cpum
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
- from the pilot RC console via RM, 2,4d/Hz channel
- control of a moving object in emergency mode
- payload control
- payload feedback
- rotating platforms control in gyro stabilization mode under AP10.3 control
- 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

Specifications

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