摘要
文中在碟形飞行器非线性数学模型基础上,设计了采用变质量矩/推力矢量复合控制装置的预测控制系统,实现了复合控制的一体化设计,简化了系统设计过程。仿真结果表明,在引入执行机构饱和约束条件时,系统设计仍能够获得良好的控制性能。
Nonlinear model of flying saucer was proposed, and nonlinear predictive control system was designed based on variable-mass/ thrust-vector compound control device, the integrated compound control was realized. The simulation shows that preferable control could be obtained even with the saturation constraint of the actuator.
出处
《弹箭与制导学报》
CSCD
北大核心
2008年第2期13-15,22,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
总装预研基金资助
关键词
碟形飞行器
非线性模型
滚动优化
预测控制
flying saucer
nonlinear model
rolling optimization
predictive control
