Abstract
A self-adaptive control loop structure is proposed to maximize the maneuver performance of a flight vehicle with considerations of system constraints and stability. By regulating the overload control command according to the actuator control command, the overload and the angle of attack can reach their time-invariant upper limits on-line. This method is in a concise form and does not need extra information compared with the classical three-loop autopilot. Simulations are carried out on a nonlinear and time varying flight dynamic model. It is shown that the actuator command can remain near its allowable utmost, generating smooth-changing and real-time maximal overload and angle of attack.
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© 2023 Beijing HIWING Sci. and Tech. Info Inst
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Guo, K., Chen, S., Wei, Z., Xu, C. (2023). A Self-adaptive Control Method for Maximum Maneuvering Flight. In: Fu, W., Gu, M., Niu, Y. (eds) Proceedings of 2022 International Conference on Autonomous Unmanned Systems (ICAUS 2022). ICAUS 2022. Lecture Notes in Electrical Engineering, vol 1010. Springer, Singapore. https://doi.org/10.1007/978-981-99-0479-2_315
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DOI: https://doi.org/10.1007/978-981-99-0479-2_315
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