Abstract
Aiming at the flight safety problems caused by the aircraft control surface failure, a control distributor for multi control surface aircraft is designed to deal with the typical failure modes of aircraft rudder surface, such as locked, floating and damaged, with the purpose of improving aircraft safety. In this paper, the control distributor is designed by transforming the different fault types into different virtual instructions and combining with the residual control allocation matrix. Based on the F-16 scale model, the simulations of the fault reconstruction algorithm under the three conditions of locked rudder surface, floating rudder surface and damaged rudder surface are carried out, so that the three-axis angle rates and control surface responses can be obtained. The simulation results are compared with the results without fault reconstruction, and the simulation results show that the fault reconstruction method is reasonable and effective, the fault reconstruction method proposed in this paper has certain engineering application value.
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References
Xiaoguang, W., Jun, D., Shuguang, L., Xiaoben, L.: The Evaluation of UAVs’ Combat Effectiveness. 1st edn. Northwestern Polytechnical University Press, Xi’an (2021)
Zhang, X., Mu, R., Chen, S.: Hybrid multi-objective control allocation strategy for reusable launch vehicle in re-entry phase. Aerosp. Sci. Technol. 116(8), 825–834 (2021)
Zhang, Z., Zhang, X., Wang, J.: An IDLC landing control method of carrier-based aircraft based on control allocation of multiple control surfaces. Acta Aeronautica et Astronautica Sinica 42(8), 525840–1–525840–16 (2021)
Sun, C.: Research on Control Allocation Based on Grey Wolf Optimizer Algorithm for the Multi-Effectors UAV. Shandong University of Science and Technology, Shandong (2020)
Sarah, P., Madruga, A.: Aerodynamic effects compensation on multi-rotor UAVs based on a neural network control allocation approach. IEEE/CAA J. Automatica Sinica 9(2), 295–312 (2022)
Zhou, Y., Chen, Y., Dong, X.: Fault reconfiguration control allocation for over-actuated aircraft based on the controllability degree. Flight Dynamic 36(5), 34–38 (2018)
Wei, Q., Chen, Z.: Control law reconfiguration under control surface failure for nonlinear aircraft dynamic. J. Beijing University of Aeronautics Astronautics 29(5), 428–433 (2003)
Yang, W., Wang, D., Wang, Y.: L1 adaptive reconfiguration controller for aircraft control effector failures. Ordnance Industry Automation 36(5), 4–8 (2017)
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Xiaoguang, W., Du, J., Wentong, J., Shuguang, L., Yongxi, L. (2023). A Fault Reconstruction Method for Aircraft with Multiple Control Surfaces. In: Yan, L., Duan, H., Deng, Y. (eds) Advances in Guidance, Navigation and Control. ICGNC 2022. Lecture Notes in Electrical Engineering, vol 845. Springer, Singapore. https://doi.org/10.1007/978-981-19-6613-2_453
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DOI: https://doi.org/10.1007/978-981-19-6613-2_453
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