AP 10.2

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

OVERVIEW

The AP 10.2 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 AP 10.2 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

KEY FEATURES

  • Very small size and lightweight
  • ESD protection
  • 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

Aluminium 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

AP 10.2 system configuration for helicopter example:

Basic modules of AP 10.2 system:

Central Processing Unit

Pitot Tube Mini

GPS Unit Mini

Onboard Telemetry Unit Mini

Servo drive SD3

AP10.2 KIT

#

Item

Designation

Part number

Weight, g

1

AP 10.2 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)

Cell
Cell
Cell

2.2

Emergency Rescue System ERS-25 (ballistic)

Cell
Cell
Cell

2.3

Video transmission channel (30 km range, FullHD, 1 Watt)

Cell
Cell
Cell

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

Download brochure (.PDF)

Download archive 3D-models (.STEP)

Download archive drawings (.PDF)

UAVOS

541 Jefferson Ave, Ste 100 Redwood City, 94063, California, USA
Email: uavos@uavos.com

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