Progress in reentry trajectory planning for hypersonic vehicle

被引:37
|
作者
Zhao, Jiang [1 ]
Zhou, Rui [1 ]
Jin, Xuelian [2 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Beijing Microelect Technol Inst, Beijing 100076, Peoples R China
基金
中国国家自然科学基金;
关键词
hypersonic vehicle; reentry trajectory planning; onboard planning; reentry trajectory optimization; footprint; QUASI-EQUILIBRIUM GLIDE; COSTATE ESTIMATION; PSEUDOSPECTRAL METHOD; GENETIC ALGORITHM; RAPID GENERATION; OPTIMIZATION; ENTRY; COLLOCATION; FRAMEWORK; WAYPOINT;
D O I
10.1109/JSEE.2014.00073
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The reentry trajectory planning for hypersonic vehicles is critical and challenging in the presence of numerous nonlinear equations of motion and path constraints, as well as guaranteed satisfaction of accuracy in meeting all the specified boundary conditions. In the last ten years, many researchers have investigated various strategies to generate a feasible or optimal constrained reentry trajectory for hypersonic vehicles. This paper briefly reviews the new research efforts to promote the capability of reentry trajectory planning. The progress of the onboard reentry trajectory planning, reentry trajectory optimization, and landing footprint is summarized. The main challenges of reentry trajectory planning for hypersonic vehicles are analyzed, focusing on the rapid reentry trajectory optimization, complex geographic constraints, and cooperative strategies.
引用
收藏
页码:627 / 639
页数:13
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