未找到相关数据
LAUNCH VEHICLE TRAJECTORY OPTIMIZATION
被引：9
作者：
ADIMURTHY, V
机构：
[1] Vikram Sarabhai Space Centre, Trivandrum, 695022, India
关键词：
SPACECRAFT - Orbits and Trajectories;
D O I：
10.1016/0094-5765(87)90039-7
中图分类号：
V [航空、航天];
学科分类号：
08 ;
0825 ;
摘要：
A launch vehicle trajectory optimization software is developed using diagonalized multiplier approach. A new modification, in which the Kuhn-Tucker vector norm is minimized along the multiplier update direction, avoids violent initial multiplier corrections. The optimality of the solutions is established, and robustness of the package demonstrated. This package is presently employed as a standard tool for mission design studies at the Indian Space Research Organisation.
引用
收藏
页码：845 / 850
页数：6
相关论文