Research on Powered Phase Guidance Method of Ballistic Missile Based on MPSP

References

[1] Hongyu Zhou, Xiaogang Wang, Naigang Cui. (2019). Glide trajectory optimization for hypersonic vehicles via dynamic pressure control [J]. Acta Astronautica, 2019, 164.

[2] Haibo Ji, LeiWang. (2019). Trajectory Tracking Strategy for Gliding Hypersonic Vehicle with Aileron Stuck at an Unknown Angle [J]. Journal of Beijing Institute of Technology, 2019, 28(03): 447-455.

[3] Zhao Jisong, Zhang Jianhong, Li Shuang. (2019). Rapid and High-Accuracy Approach for Hypersonic Glide Vehicle Reentry Trajectory Optimization [J]. Journal of Astronautics, 2019, 40(09): 1034-1043.

[4] Yao Zhang, Xiao Wang, Shengjing Tang. (2019). A globally fixed-time solution of distributed formation control for multiple hypersonic gliding vehicles [J]. Aerospace Science and Technology, 2019.

[5] Kun Zhao, DengQing Cao, WenHu Huang. (2018). Maneuver control of the hypersonic gliding vehicle with a scissored pair of control moment gyros [J]. Science China Technological Sciences, 2018, 61(8).

[6] Jianwen Zhu, Ruizhi He, Guojian Tang,Weimin Bao. (2018). Pendulum maneuvering strategy for hypersonic glide vehicles [J]. Elsevier Masson SAS, 2018, 78.

[7] Oza, H. B. and Padhi, R. (2012). Impact-Angle-Constrained suboptimal model predictive static programming guidance of air-to-ground missiles [J]. Journal of Guidance, Control, and Dynamics, 2012, 35(1): 153-164.

[8] Arnab Maity, Harshal B., Oza and Radhakant Padhi. (2013). Generalized model predictive static programming and its application to 3D impact angle constrained guidance of Air-to-Surface missiles [C]. 2013 American Control Conference (ACC), Washington, DC, USA, 2013: 4999-5014.