首页> 外文会议>International Symposium on Instrumentation and Control Technology; 20061013-15; Beijing(CN) >Design of Robust Controller Based on Adaptive Backstepping and Slide Mode for Flight Simulator
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Design of Robust Controller Based on Adaptive Backstepping and Slide Mode for Flight Simulator

机译:基于自适应Backstepping和滑模的飞行仿真器鲁棒控制器设计。

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Considering unknown nonlinearities, external disturbances and parameter perturbations existing in the flight simulator, A backstepping and slide mode controller is designed for the flight simulator. Firstly, the dynamic model of the flight simulator is proposed by test. Secondly, the backstepping controller with friction parameter update law is deduced for this dynamic model. Finally, simulation results show that the output from the system can achieve asymptotic tracking of the given position reference signal and the aberration of velocity response under the control of common PID controller is overcome.
机译:考虑到飞行模拟器中存在未知的非线性,外部干扰和参数扰动,为飞行模拟器设计了后推和滑模控制器。首先通过试验提出了飞行模拟器的动力学模型。其次,针对该动力学模型推导了具有摩擦参数更新律的反推控制器。最后,仿真结果表明,该系统的输出可以实现对给定位置参考信号的渐近跟踪,并且克服了在普通PID控制器的控制下速度响应的畸变。

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