Research Article
Study and Hardware-in-the-Loop Simulation of Flight Mach Control System Based on Fuzzy Control Theory
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@INPROCEEDINGS{10.1007/978-3-030-32216-8_52, author={Gan Cui and Huiqiang Zhang}, title={Study and Hardware-in-the-Loop Simulation of Flight Mach Control System Based on Fuzzy Control Theory}, proceedings={Simulation Tools and Techniques. 11th International Conference, SIMUtools 2019, Chengdu, China, July 8--10, 2019, Proceedings}, proceedings_a={SIMUTOOLS}, year={2019}, month={10}, keywords={Unmanned Aerial Vehicle Flight Mach number Fuzzy control Hardware-in-the-loop simulation}, doi={10.1007/978-3-030-32216-8_52} }- Gan Cui
Huiqiang Zhang
Year: 2019
Study and Hardware-in-the-Loop Simulation of Flight Mach Control System Based on Fuzzy Control Theory
SIMUTOOLS
Springer
DOI: 10.1007/978-3-030-32216-8_52
Abstract
An efficient and reliable flight Mach controller is specially needed for an Aircraft. A Flight Mach Fuzzy Controller (FMFC) based on modern Fuzzy control theory is designed for an Unmanned Aerial Vehicle (UAV) using a turbojet engine. The theory and process of designing control law is introduced and its control performance is optimized by changing the scaling factor. In order to evaluate the control performance, the mathematical simulation and hardware-in-the-loop simulation are carried out respectively, and the simulation results are compared. The evaluation shows good control performance to stabilize the UAV flight Mach number to the target Mach number quickly by controlling the engine work condition.
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