AP10.2

Automatic Control System for UAV with a takeoff weight of 15 kg up to 100 kg

Overview

The AP10.2 system is designed to control a surface, ground or airborne platform automatically, semi-automatically or manually.

The system is configurable for the following platforms:
  • Standard airplane for automatic take-off and landing
  • Rotor-wings for automatic take-off and landing
  • Balloons, Blimps
  • USVs (boats)
  • UGVs (cars)
The AP10.2 was designed for small platforms and has the following advantages:
  • reduced form factors (avionics weight less then 350 g)
  • reduced energy consumption
Most payload can be interfaced through:
  • 1-Wire
  • RS-232
  • RS-485
  • TTL UART
  • CAN

Main functions

  • Very small size and lightweight
  • ESD protection, -40..+80C operation
  • Leading edge components and technologies
  • Dead-reckoning, flight and navigation without GPS
  • Automatic take-off and automatic landing
  • Operating/flight mechanisms controls
  • Engine/power plant control
  • Semi-automatic control with automatic stabilization
  • Manual control over 928MHz from ground control station
  • Emergency mode
  • Payload control
  • Payload feedback
  • Gyro-stabilization mode for rotating platforms
  • Telemetry 10Hz with compressed stream, 100km LOS
  • Ground simulation mode – flight simulator
  • Operator training on flight simulator
  • Pre-flight and flight assignment testing
  • Onboard power control and monitoring
  • Power stabilization
  • Distribution, including emergency power supply mode

Specifications

Interfaces and characteristics:

  • 12x servo drives (PWM outputs)
  • 12x RPM sensor inputs (hall effect sensor)
  • 1-Wire interface
  • TTL UART interface
  • RS-485 interface
  • Controller area network - CAN
  • RS-232 interface
  • 4x Active-ground switched power output (4.7a, @ 27V, 68mOhm)
  • 12x digital inputs (timing, level)
  • 12x general purpose inputs-outputs (remappable on MCU)

Technical specifications:

Operating temperature IP rating Housing material Connector
-40°C to +60°C IP67 Aluminum alloy Harwin m300-3240696M1
Amphenol PTO2E14-19P
Amphenol PT02E8-4P
Harwin M80-9420605
Power supply Protection
7-27 V Gated logic on all digital IO pins ESD protection Power supply reverse-polarity protection

 

Application cases

Aircraft

Helicopter

AP10.2 system configuration for helicopter example:

Basic modules of AP10.2 system:

Central Processing Unit Pitot Tube Mini
bcpm-cpum pitot
GPS Unit Mini Onboard Telemetry Unit Mini Servo drive SD3
bcpm-cpum pitot pitot

 

AP10.2 Package

# Item Designation Part number Weight, g
 1 AP10.2 Kit
 1.1 Central Processing Unit  CPU  UV.431329.102.330  160
 1.2 Onboard Telemetry Unit Mini  OTUM  UV.468339.100.311  120
 1.3 Pitot Tube Mini  PTM  UV.468339.90.345  74
 1.4 GPS Receiver Mini  GPSM  UV.431329.102.365  49
 All housings are hermetic.
 2 Optional airborne equipment   
 2.1 Laser Altimeter (0-100 m altitude)      
 2.2 Emergency Rescue System ERS-25 (ballistic)      
 2.3 Video transmission channel (30 km range, FullHD, 1 Watt)      
 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 Portable ground control station *  PGCS  UV.468323.01  19500

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

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UAVOS INC

465 N Whisman Rd # 600 Mountain View CA 94043 USA

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