Leap trajectory tracking control based on sliding mode theory for hypersonic gliding vehicle
Author:
Publisher
Zhejiang University Press
Subject
General Engineering
Link
https://link.springer.com/content/pdf/10.1631/jzus.A2100362.pdf
Reference33 articles.
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2. An K, Guo ZY, Xu XP, et al., 2020. A framework of trajectory design and optimization for the hypersonic gliding vehicle. Aerospace Science and Technology, 106:106110. https://doi.org/10.1016/j.ast.2020.106110
3. Awad A, Wang HP, 2016. Roll-pitch-yaw autopilot design for nonlinear time-varying missile using partial state observer based global fast terminal sliding mode control. Chinese Journal of Aeronautics, 29(5):1302–1312. https://doi.org/10.1016/j.cja.2016.04.020
4. Chen K, Liang WC, Liu MX, et al., 2020. Comparison of geomagnetic aided navigation algorithms for hypersonic vehicles. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(8):673–683. https://doi.org/10.1631/jzus.A1900648
5. Chen K, Liang WC, Zeng CZ, et al., 2021. Multi-geomagnetic-component assisted localization algorithm for hypersonic vehicles. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 22(5):357–368. https://doi.org/10.1631/jzus.A2000524
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