AP10.1

Automatic Control System for UAV with a takeoff weight of 100 kg up to 1500 kg

Overview

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

Main functions

  • 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

Specifications

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

 

Application cases

Aircraft

Helicopter

Motorboat

AP10.1 system configuration for airplanes example:

Autopilot Configuration

AP10.1 Package

# 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

Request for Information about AP10.1

Click Here

Request for Information

UAVOS INC

465 N Whisman Rd # 600 Mountain View CA 94043 USA

Phone: +1 650 584-3176
Email: This email address is being protected from spambots. You need JavaScript enabled to view it.