Abstract
This paper designs the adaptive reconfiguration controller of the carrier-based aircraft landing with the single-engine failure. It mainly adopts the combination of reconstruction control and LQR, and designs an adaptive reconfiguration control law to realize a single-engine carrier aircraft gliding at a constant speed and the track correction. When the single engine fails, the landing control law of the carrier-based aircraft is switched to the control law designed in this paper. Through simulation and comparison of the classic control methods, the stable control of the single-engine landing adaptive reconstruction is realized.
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Zhang, Y., Zhou, Y., Yan, X., Yin, D. (2022). Single-Engine Landing Adaptive Reconfiguration Controller of Carrier-Based Aircraft. In: Proceedings of the 5th China Aeronautical Science and Technology Conference. Lecture Notes in Electrical Engineering, vol 821. Springer, Singapore. https://doi.org/10.1007/978-981-16-7423-5_50
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DOI: https://doi.org/10.1007/978-981-16-7423-5_50
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