Abstract
This paper proposes a decoupling control strategy for aircraft with thrust vector at high angle of attack. To eliminate strong couplings among different channels, the three-channels controllers are designed independently, respectively. The channels coupling, aerodynamic uncertainties, unmodeled dynamics, and external disturbance are regarded as generalized disturbance and extended into a new state, which is estimated and compensated in real time by extended state observer (ESO). The sliding mode control (SMC) method is employed to achieve the expected control performance. The numerical simulations demonstrate the effectiveness of the proposed control strategy.
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Liu, J., Chen, Z., Sun, M., Sun, Q. (2020). High Angle of Attack Sliding Mode Control for Aircraft with Thrust Vector Based on ESO. In: Jia, Y., Du, J., Zhang, W. (eds) Proceedings of 2019 Chinese Intelligent Systems Conference. CISC 2019. Lecture Notes in Electrical Engineering, vol 592. Springer, Singapore. https://doi.org/10.1007/978-981-32-9682-4_6
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DOI: https://doi.org/10.1007/978-981-32-9682-4_6
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