摘要
实时微分控制是进行航天器轨道控制的主要方法。本文在费景高所提出的算法基础上 ,提出了一种有效的改进算法 ,扩大了算法的适用范围。文章对算法的稳定性进行了研究 ,并给出了此算法在弹道导弹显式制导中的应用实例。
Real-time differential control is a major method to control the trajectory of spacecraft. An efficient algorithm is presented based on the algorithm presented by Fei Jinggao. The new algorithm can be used in more instances than the old one. The stability of the new algorithm is discussed in the paper.The algorithm is used in the guidance of ballistic missile in the end.
出处
《航天控制》
CSCD
北大核心
2001年第4期48-52,共5页
Aerospace Control
基金
国家高技术计划 86 3- 40 9项目资助
