Reinforcement learning adaptive risk-sensitive fault-tolerant IGC method for a class of STT missile-Reference-Cited by-同舟云学术

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Reinforcement learning adaptive risk-sensitive fault-tolerant IGC method for a class of STT missile

Published:2024-07-29 Issue:20 Volume:112 Page:18195-18218
ISSN:0924-090X
Container-title:Nonlinear Dynamics
language:en
Short-container-title:Nonlinear Dyn

Author:

Wang Zheng^ORCID,Hao Yuting

Funder

the Foundation of China National Key Laboratory of Science and Technology on Test Physics & Numerical Mathematics

the National Natural Science Foundation of China

the research project of China Academy of Launch Vehicle Technology

Publisher

Springer Science and Business Media LLC

Link

https://link.springer.com/content/pdf/10.1007/s11071-024-09776-5.pdf

Reference54 articles.

1. Lai, C., Wang, W., Zhou, B., Zhou, X., Lin, D.: Three-dimensional partial integrated guidance and control with impact angle constraints. Yuhang Xuebao/J. Astronaut. 40(8), 937–947 (2019). https://doi.org/10.3873/j.issn.1000-1328.2019.08.010

2. Bao, C., Wang, P., Tang, G.: Integrated method of guidance, control and morphing for hypersonic morphing vehicle in glide phase. Chin. J. Aeronaut. 34(5), 535–553 (2021). https://doi.org/10.1016/j.cja.2020.11.009

3. Wu, Y., Lu, X., Wang, Z.: Research on integrated design of aircraft spiral maneuver, guidance and control based on sliding mode control. Beijing Ligong Daxue Xuebao/Trans Beijing Instit Technol 42(5), 523–529 (2022). https://doi.org/10.15918/j.tbit1001-0645.2021.089

4. Wang, X., Zhang, X., Lin, P., Li, W.: Integrated strategy of penetration and attack based on optimal control. Flight Dyn. 40(06), 51-60+71 (2022). https://doi.org/10.13645/j.cnki.f.d.20220716.001

5. Xu, M., Chen, G., Wang, W.: Aero-control integrated design for reusable launch vehicle based on feedback linearization. Meas. Control Technol. 37(9), 88–91 (2018). https://doi.org/10.19708/j.ckjs.2018.09.021

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