Three-Dimensional Super-Twisting Sliding Mode Guidance Law with Impact Time and Angle Constraints
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-6613-2_410
Reference13 articles.
1. Erer, K.S., Ozgoren, M.K.: Control of the impact angle using biased proportional navigation. In: AIAA Guidance, Navigation, and Control, pp. 5113–5127 (2016)
2. Liu, B., Hou, M., Feng, D.: Nonlinear mapping based impact angle control guidance with seeker’s field-of-view constraint. Aerosp. Sci. Technol. 86, 724–736 (2019)
3. Zhang, X., Dong, F., Zhang, P.: A new three-dimensional fixed time sliding mode guidance with terminal angle constraints. Aerosp. Sci. Technol. 121, 107370 (2022)
4. Xinxin, W., Hongqian, L., Xianlin, H., Yefeng, Y., Zongyu, Z.: Three-dimensional time-varying sliding mode guidance law against maneuvering targets with terminal angle constraint. Chin. J. Aeronaut. 35(4), 303–319 (2022)
5. Yang, T., Xiaoping, Z., Zhou, Z., Fei, Y.: Two-phase guidance law for impact time control under physical constraints. Chin. J. Aeronaut. 33(11), 2946–2958 (2020)
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