Fixed-wing model for aircraft flight control auto-stabilization system

Hua Li

doi:10.1117/12.3030294

5 June 2024 Fixed-wing model for aircraft flight control auto-stabilization system

Hua Li

Proceedings Volume 13163, Fourth International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024); 1316370 (2024) https://doi.org/10.1117/12.3030294
Event: International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024), 2024, Xi'an, China

Abstract

This design takes the remote-controlled fixed-wing model aircraft as the platform, uses the STM32 micro controller as the main control chip, and uses the MPU6050 sensor to collect attitude information during the flight of the fixed-wing model aircraft to increase the anti-interference of the model aircraft. In order to achieve the purpose of lowering the threshold for beginners to learn aircraft model sports. In terms of stabilizing the flight attitude of the model aircraft, the acceleration and angular velocity are used for feedback. After many in-depth optimizations, users can perform pure manual flight and self-stabilization mode flight by switching to the auto-stabilization mode, which not only helps beginners to learn, but also greatly improves the safety and ability of the model aircraft.

(2024) Published by SPIE. Downloading of the abstract is permitted for personal use only.

Citation Download Citation

Hua Li "Fixed-wing model for aircraft flight control auto-stabilization system", Proc. SPIE 13163, Fourth International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024), 1316370 (5 June 2024); https://doi.org/10.1117/12.3030294

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