研究目的
To design and implement a semi-physical simulation instrument system based on virtual reality and microcontroller technologies for a light-duty electric aircraft simulator, meeting its demands and providing a reference for other aircraft simulators.
研究成果
The developed instrument system meets the demands of the light-duty electric aircraft simulator with real effect, stable operation, and fine fidelity. It serves as a valuable reference for developing instrument systems for other aircraft simulators.
研究不足
The system's performance is dependent on the accuracy of the virtual instrument models and the reliability of the hardware components. Potential areas for optimization include enhancing the fidelity of instrument simulations and improving the robustness of hardware signal processing.
1：Experimental Design and Method Selection:
The system combines virtual instrument technology and microcontroller technology for semi-physical simulation.
2：Sample Selection and Data Sources:
Flight data and dashboard operation signals are inputs; display information of the virtual instrument and panel indicator status are outputs.
3：List of Experimental Equipment and Materials:
Includes GL Studio and VC++
4：0 platforms for software development, and STC90C52 microcontroller for hardware. Experimental Procedures and Operational Workflow:
Development of virtual instruments on GL Studio platform, hardware design for signal processing, and system integration with flight-computing system.
5：Data Analysis Methods:
Performance testing through network communication using UDP protocol.
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