摘要
针对飞行器在行星表面软着陆问题 ,利用变结构系统中滑动模态的思想 ,设计了鲁棒控制律 ,并对工程上的实现进行了讨论 ,得到了简单、实用的控制律 ,仿真研究说明了方法的有效性。
For flight vehicle soft landing on certain planet, robust control law is designed based on the technique of sliding modes in variable structure systems, the realization of the control law in engineering is discussed, and as a result, a simple and practical control law is developed. Simulation research justifies the feasibility of the proposed method.
出处
《导弹与航天运载技术》
北大核心
2001年第2期39-43,共5页
Missiles and Space Vehicles
