中国航天（英文版）2016，Vol.17Issue(2)：3-8,6.
An Improved United Trajectory Optimization Approach in Boost-phase Considering Attitude Control Ability
An Improved United Trajectory Optimization Approach in Boost-phase Considering Attitude Control Ability
MA Baohai 1WANG Zhi 1SONG Lei 1WANG Xiaojun1
作者信息
- 1. Beijing Institute of Aerospace Systems Engineering, Beijing 100076
- 折叠
摘要
关键词
Lower trajectory/Trajectory design/United optimization/SQPKey words
Lower trajectory/Trajectory design/United optimization/SQP引用本文复制引用
MA Baohai,WANG Zhi,SONG Lei,WANG Xiaojun..An Improved United Trajectory Optimization Approach in Boost-phase Considering Attitude Control Ability[J].中国航天（英文版）,2016,17(2):3-8,6.
