摘要
建立了无人动力伞6自由度控制模型,依托该模型分析了系统的动力学特性与动态性能,阐述了基于预测控制算法的无人动力伞系统飞行控制律,并在实际飞行条件下,验证飞行控制系统的控制精度。
The paper develops a six degree-of-freedom model of unmanned powered parafoil to analyze the dynamics and kinematics of the parafoil system.Model predictive control is proposed as a control strategy,which is suitable for optimizing the performance of powered parafoil.The feasibility and control accuracy of the control law are verified in the flying experiment.
出处
《军械工程学院学报》
2011年第2期52-55,共4页
Journal of Ordnance Engineering College
基金
军队科研计划项目
关键词
无人动力伞系统
预测控制
建模
unmanned powered parafoil
predictive control
modeling
