Rapid Trajectory Planning for Asteroid Landing with Thrust Magnitude Constraint

被引：17
|
作者：
Yang, Hongwei [1 ,2 ]
Bai, Xiaoli [2 ]
Baoyin, Hexi [1 ]
机构：
[1] Tsinghua Univ, Sch Aerosp Engn, Beijing 100084, Peoples R China
[2] Rutgers State Univ, Dept Mech & Aerosp Engn, Piscataway, NJ 08854 USA
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2017年 / 40卷 / 10期
基金：
中国国家自然科学基金;
关键词：
GUIDANCE; GENERATION; OPTIMIZATION; NAVIGATION;
D O I：
10.2514/1.G002346
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
收藏
页码：2713 / 2720
页数：8
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