GCS/LCS (Ground/Launch Control System)
Feature
Ground control system for the RQ-101 is composed of a flight control assembly and an integrated arithmetic operation assembly. Perform the function of flight control, mission planning, target tracking, and image acquisition using additional equipment such as knob assembly, switch assembly, contact indicator, and flight controller located in the flight control assembly.

 

Spec
  • pilot, navigation, observer bay
  • real-time data communication
  • real-time video communication
  • switch assembly
  • knob assembly
  • mission control display
  • external pilot box
  • C-BAND/UHF communication interlock
  • uplink/downlink data interlock

 

 

PBX (Pilot Box)
Feature
Pilot Box is External manipulator for unmanned aircraft which linked with the ground control system by RS-422 communication. With RS-422 communication, throttle, rudder, elevation and aileron of aircraft can be controlled directly. The switch located at the top allows switching to automatic / manual control, and the data being controlled can be checked through the front panel display.

 

Spec
  • RS-422 communication
  • flight control switch
  • throttle, rudder, elevation, aileron control stick
  • break stick
  • LED display

 

 

HQS (Handling Quality Simulator)
Feature
HQS provides an engineering system test environment for the FBW Helicopter automatic flight control system that can generate data necessary for the HILS system and verify its design results by interface with the servo model and aircraft equipment. 3-channel display screen is provided for flight control analysis and is provided flight test environment according to ADS-33 criteria to precise flight control performance.

 

Spec
  • pilot cockpit
  • 3 channel image generator
  • real-time host computer
  • real-time signal interface system
  • simulator control desk
  • ADS-33 MTE test course

 

 

AFCS HILS (Auto Flight Control System HILS)
Feature
AFCS HILS provides an engineering system test environment for the LCH automatic flight control system that can generate data necessary for the HILS system and verify its design results by interface with the servo model and aircraft equipment. 3-channel display screen is provided for flight control analysis and is provided flight test environment according to ADS-33 criteria to precise flight control performance.

 

Spec
  • real-time simulation computer system
  • real-time signal I/O system
  • 3 channel display system (screen & projectors)
  • control loading system 4 axes, including mechanical linkage
  • simulator control desk
  • ADS-33 MTE test course

 

 

GTE (Ground Test Equipment)
Feature
Ground Test Equipment(GTE) can perform unit and integrated testing of external interfaces such as MIL-STD-1553B, Discrete, and Analog, etc. Also provides the ability to check whether the performance requirements are satisfied through simulated aircraft system signal.

 

Spec
  • MIL-STD-1553B communication Test
  • analog I/O signal test
  • discrete I/O signal test
  • video processing test
  • audio processing test
  • power test
  • aircraft interface data simulation

 

 

GSE (Ground Support Equipment)
Feature
Ground support equipment provides a various of support functions for system operations such as flight simulation, mission planning data creation, mission debriefing, flight data analysis, software update, and integrated function test according to the customers requirements.

 

Spec
  • flight simulation (using HOTAS)
  • mission planning
  • mission debriefing
  • flight data analysis
  • electrical interface simulation
  • functional requirement test