贾杰, 曹琦, 谢宇, 张向阳. 基于双环滑模的导弹控制系统设计与仿真[J]. 南昌航空大学学报(自然科学版), 2009, 23(4): 6-9.
引用本文: 贾杰, 曹琦, 谢宇, 张向阳. 基于双环滑模的导弹控制系统设计与仿真[J]. 南昌航空大学学报(自然科学版), 2009, 23(4): 6-9.
shu
JIA Jie, CAO Qi, XIE Yu, ZHANG Xiang-yang. A Missile Control System Design and Simulation Based on Double-loop Sliding Mode Control[J]. Journal of nanchang hangkong university(Natural science edition), 2009, 23(4): 6-9.
Citation: JIA Jie, CAO Qi, XIE Yu, ZHANG Xiang-yang. A Missile Control System Design and Simulation Based on Double-loop Sliding Mode Control[J]. Journal of nanchang hangkong university(Natural science edition), 2009, 23(4): 6-9.
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基于双环滑模的导弹控制系统设计与仿真

A Missile Control System Design and Simulation Based on Double-loop Sliding Mode Control

    摘要
  • 摘要: 基于滑动模态控制理论设计了一种导弹姿态控制器,这个控制器应用双环滑模控制的方案,可以获得对角速度及姿态角的同时跟踪并具有较好的鲁棒性能和解耦性能.仿真结果表明,该控制系统具有良好的跟踪性能和鲁棒性.

     

    Abstract: A missile attitude-control controller was designed on the base of sliding mode control(SMC) theory.Double-loop SMC scheme was utilized,and this controller obtains the track of both the angular velocity and attitude angle,and it has higher robustness and decoupling.The result of simulation analysis show that this control system has very good tracing performance and robustness.

     

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