摘要
针对碟形飞行器设计了基于线性优化方法的预测控制系统,实现了变质量矩/推力矢量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,这一设计能够获得良好的控制性能.
Predictive control system based on linear optimization method is designed.The system is integrated the design of moving-mass/thrust-vectoring compound control,and the design process is simplified.Simulation results show that preferable control results can be obtained with the design.
出处
《战术导弹技术》
北大核心
2008年第3期66-69,共4页
Tactical Missile Technology
关键词
碟形飞行器
线性化
滚动优化
预测控制
flying saucer
linearization
rolling optimization
predictive control
