鲁棒逆动态估计技术在飞行器控制中的应用  

Application of A Robust inverse Dynamics Estimation Theory to the Aircraft Control

作　　者：魏文领 张新国[1] 刘林[1] 

机构地区：[1]飞行自动控制研究所,西安710065

出　　处：《弹箭与制导学报》2006年第S2期350-352,356,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：分析鲁棒逆动态估计(RIDE)方法的基本原理和控制器的设计方法,利用飞行器的线性化模型,求得控制器的各个增益,同时,利用动压对其进行调参。仿真表明,该方法能有效地应用于某飞行器的纵向控制。The basic theory and design method of the controller of a Robust Inverse Dynamics Estimation control system are analysed in this paper.The gains in the controller are got by using the linearized model,and a dynamic pressure scheduler was used to schedule the gains of the controller.The simulation results show that the method can be effective- ly use in the aircraft longitudinal control.

关 键 词：鲁棒逆动态估计 伪微分反馈动压调参 相似变换 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]