摘要
给出了在等周约束条件下确定性动态系统最优控制问题的数学提法和求解原理；讨论了探空火箭在真空中飞行达给定弹道顶点高度时起飞质量为最小的推力程序。
This paper deals with the multistage optimal control problem with restrictive condition,gives the basic mathematical formulation of this problem and its solving principle,discusses the optimal thrust programme in Vacuum for minimun launching mass of two stage sounding rocket in the given maximum flight altitude.
出处
《中国空间科学技术》
EI
CSCD
北大核心
1998年第1期25-29,44,共6页
Chinese Space Science and Technology
