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Three axis electronic flight motion simulator real time control system design and implementation.

Zhiyuan Gao1, Zhonghua Miao1, Xuyong Wang2

  • 1School of Mechatronic Engineering and Automation, Shanghai University, Shanghai, 200072, People's Republic of China.

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This paper presents a three-axis electronic flight motion simulator for inertial navigation system testing. The developed real-time control system demonstrates effective dynamic and static performance for high-precision applications.

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Area of Science:

  • Aerospace Engineering
  • Control Systems Engineering
  • Robotics

Background:

  • Inertial navigation systems (INS) require robust testing platforms.
  • Existing flight motion simulators may lack precision or real-time control capabilities.
  • Advanced simulation is crucial for developing high-performance INS.

Purpose of the Study:

  • To report the design and implementation of a three-axis electronic flight motion simulator.
  • To develop and validate a real-time control system for the simulator.
  • To demonstrate the simulator's suitability for inertial navigation testing.

Main Methods:

  • Simulator modeling and controller design.
  • Hardware implementation of the flight motion simulator.
  • Development of a real-time control system addressing issues like time unification and high-speed signal processing.

Main Results:

  • Successful implementation of a three-axis electronic flight motion simulator.
  • A real-time control system was designed and tested.
  • The system achieved good dynamic and static performances for inertial navigation applications.

Conclusions:

  • The proposed flight motion simulator and its real-time control system are effective.
  • The simulator provides a valuable tool for inertial navigation system testing.
  • The system exhibits promising performance for high-precision INS development.