Robust Sliding Mode Control for Hypersonic Cruise Missile Using Dynamic Pressure Feedback
Author:
Xu HongyangORCID, Li Hongjun, Fang Guicai, Fan Yonghua
Publisher
Springer Singapore
Reference13 articles.
1. Zhao, Z.T., Huang, W., Yan, L., Yang, Y.G.: An overview of research on wide-speed range waverider configuration. Prog. Aerosp. Sci. 113, 1–14 (2020) 2. Spravka, J.J., Jorris, TR.: Current hypersonic and space vehicle flight test and instrumentation. In: AIAA Flight Testing Conference. AIAA, Dallas, JU (2015) 3. Wang, X.M., Xie, R., Zhang, Y.M., Li, B., Wang, J.: A survey of the hypersonic flight vehicle and its guidance and control technology. J. Harbin Inst. Technol. 51(3), 1–14 (2019) 4. Xu, B., Shi, Z.K., Sun, F.C., He, W.: Barrier Lyapunov function based learning control of hypersonic flight vehicle with AOA constraint and actuator faults. IEEE Trans. Cybern. 49(3), 1047–1057 (2019) 5. Xu, H.Y., Fan, Y.H., Tong, X., Yan, J.: Designing control system of hypersonic vehicle with dynamic pressure constraints considered. J. Northwest. Polytechnical Univ. 37(1), 41–47 (2019)
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