摘要
针对直接力/气动力复合控制飞行器的姿态控制系统设计方法进行了研究,总结了直接力、气动力协同工作方法,分析了直接力、气动力子系统控制律设计方法的特点,详细介绍了直接力子系统中的侧喷发动机点火方式及点火算法,阐述了复合控制系统稳定性分析的现有方法,对直接力/气动力复合控制技术发展趋势进行了展望,为复合控制系统设计提供参考。
A survey on the design methods of attitude control system for compound control aircraft with lateral thrusters and aerodynamic fins is proposed. At first, the cooperative working method between lateral thrust and aerodynamic force is summarized.Then the design method of control law for lateral thrust and aerodynamic force subsystems is analyzed. The ignition mode and ignition algorithm of lateral thrusters required to implement commands are introduced in detail. Additionally, the stability analysis method of compound control system is discussed. Finally, the development trend of compound control technology is prospected. A reference for the design of compound control system is provided.
引文
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