摘要
为了提高巡航导弹的生存能力，使其能够跟踪地形起伏飞行，提出了用二自由度Ｗｉｅｎｅｒ－Ｈｏｐｆ最优化方法设计地形跟踪控制器。仿真结果表明，该方法具有良好的跟踪性能。另外，针对反馈通道气压式高度表的延迟问题，提出了气压—惯性方案，并进行了仿真验证。
Adopts two-degree-of-freedom Wiener-Hopf optimal method to design a cruise missile's terrain following controller, in order to improve its viability. The simulation results evince that the offered method has a favourable terrain following performance. And presents an altimeter-inertia scheme, which is validated by simulation, to deal with the time delay of baric altimeter in feedback loop.
出处
《航天控制》
CSCD
北大核心
1998年第3期30-35,共6页
Aerospace Control
