| 论条件最优控制问题 |
| |
| 引用本文： | 李大治,李大耀.论条件最优控制问题[J].中国空间科学技术,1998,18(1):25-29,44. |
| |
| 作者姓名： | 李大治 李大耀 |
| |
| 作者单位： | 南通医学院(李大治)，北京空间机电研究所(李大耀) |
| |
| 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妥原理；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。
|
| 关 键 词： | 最佳控制 动态特性 探空火箭 条件最优 |
ON OPTIMAL CONTROL PROBLEM WITH RESTRICTIVE CONDITION |
| |
| Li Dazhi.ON OPTIMAL CONTROL PROBLEM WITH RESTRICTIVE CONDITION[J].Chinese Space Science and Technology,1998,18(1):25-29,44. |
| |
| Authors: | Li Dazhi |
| |
| Abstract: | 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. |
| |
| Keywords: | Optimal control Dynamic characteristic Sounding rocket |
| 本文献已被 CNKI 维普 等数据库收录！ |
