Abstract
Based on backstepping design, a strongly robust adaptive control system is designed for reentry attitude of near space hypersonic vehicle, which is suffered by parameter uncertainties and external disturbances. In each step of backstepping design, the unknown upper bound of uncertainty is estimated by adaptive method to reduce conservation. The derivative of the virtual controller is calculated by a precise differentiator based on higher-order sliding modes. Using non-quadratic Lyapunov function, the global asymptotic stability of the closed-loop system is proved. Simulation results show that the proposed control system can overcome the impact of lage-scale perturbations of aerodynamic parameters and external disturbances, which has better dynamic qualities, tracking capabilities compared to the traditional backstepping controller.
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References
Jie, H., Dezhai, Z.: Characteristics and key technology research for hypersonic vehi-cle. In: Aerospace Science and Technology Innovation and the Yangtze River Delta Economic Transformation Development BBS, pp. 227–231 (2012)
Shaughnessy, J.D., Pinckney, S.Z., McMinn, J.D., et al.: Hypersonic vehicle simulation model: winged-cone configuarion. NASA TM-102610 (1990)
Kanellakopoulos, I., Kokotovic, P.V., Stephen Morse, A.: Systematic design of adaptive controllers for feedback linearizable systems. IEEE Transactions on Automatic Control 36(11), 1241–1253 (1991)
Koshkouei, A.J., Zinober, A.S.I.: Adaptive backstepping control of nonlinear systems with unmatched uncertainty. In: Proceedings of the 39th IEEE Conference on Decision and Control, Sydney, Australia, pp. 4765–4770 (December 2000)
Swaroop, D., Hedrick, J.K., Yip, P.P., Gerdes, J.C.: Dynamic surface control for a class of nonlinear systems. IEEE Transactions on Automatic Control 45(10), 1893–1899 (2000)
Gao, D., Sun, Z., Du, T.: Dynamic surface control for hypersonic aircraft using fuzzy logic system. In: Proceeding of IEEE International Conference on Automation and Logistics, Jinan, pp. 2314–2319 (2007)
Zhou, Y., Wu, Y., Hu, Y.: Robust backstepping sliding mode control of a class of uncertain MIMO nonlinear systems. In: 2007 IEEE International Conference on Control and Automation, Guangzhou, pp. 1916–1921 (2007)
Zhu, K., Qi, N., Qin, C.: Adaptive sliding mode controller design for BTT missile based on backstepping control. Journal of Astronautics 31(3), 769–773 (2011)
Levant, A.: Higher-order sliding modes, differentiation and output-feedback control. International Journal of Control 76(9/10), 924–941 (2003)
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Zhang, J., Sun, C., Zhang, R., Qian, C., Xue, L. (2013). Adaptive Backstepping Controller Design for Reentry Attitude of Near Space Hypersonic Vehicle. In: Sun, C., Fang, F., Zhou, ZH., Yang, W., Liu, ZY. (eds) Intelligence Science and Big Data Engineering. IScIDE 2013. Lecture Notes in Computer Science, vol 8261. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-42057-3_81
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DOI: https://doi.org/10.1007/978-3-642-42057-3_81
Publisher Name: Springer, Berlin, Heidelberg
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