Controlling system design for flight atmospheric parameter test

Manghe Geng; Tao Xu; Hexuan Zhang

doi:10.1117/12.2679950

18 July 2023 Controlling system design for flight atmospheric parameter test

Manghe Geng, Tao Xu, Hexuan Zhang

Proceedings Volume 12722, Third International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2023); 1272251 (2023) https://doi.org/10.1117/12.2679950
Event: International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2023), 2023, Hangzhou, China

Abstract

In response to the need for calibration of airborne air data equipment, a flight air parameter test system based on STM32F103C8T6 single-chip microcomputer and closed-loop pressure control is designed. The host device is a PC, and the client device is a control system composed of STM32F103C8T6 single-chip microcomputer. The host computer develops controlling system software with LabVIEW. As the kernel module, STM32F103C8T6 single-chip microcomputer is chosen to design the client computer circuit. Besides, this paper designs the adjustable voltage output circuit with TLV5630, the power module, the switch controlling circuit with the relay module, the PWM module with the IO port of STM32F103C8T6 and the RS232 communication circuit with SP3232. Finally, the effectiveness of the controlling system is illustrated by the software.

Citation Download Citation

Manghe Geng, Tao Xu, and Hexuan Zhang "Controlling system design for flight atmospheric parameter test", Proc. SPIE 12722, Third International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2023), 1272251 (18 July 2023); https://doi.org/10.1117/12.2679950

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