Pseudo-spectral Trajectory Optimization Method with Constraint on the Change Rate of Control Variables

被引:0
|
作者
Zhao, Jisong [1 ]
Shang, Teng [2 ]
Zhang, Jinming [1 ]
Cheng, Xiaoming [2 ]
Liu, Jiaolong [2 ]
机构
[1] College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
[2] Beijing Aerospace Automatic Control Institute, Beijing,100854, China
来源
Yuhang Xuebao/Journal of Astronautics | 2022年 / 43卷 / 10期
关键词
Compilation and indexing terms; Copyright 2024 Elsevier Inc;
D O I
暂无
中图分类号
学科分类号
摘要
Aerodynamics - Electronic guidance systems - Finite difference method - Guided missiles - Spectroscopy - Trajectories
引用
收藏
页码:1368 / 1377
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