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

    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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