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Research on Optimal Sliding Mode Pose Control for a Six-DOF Air-Bearing Simulation Platform System

机译:六自由度航空仿真平台系统最优滑模姿态控制研究

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摘要

According to the requirements of the ground experiment table which is designed to simulate the lunar orbiter's docking and the sample transferring processes for the 3rd step of China's Lunar Exploration Program, a 6-DOF air-bearing simulation platform system is designed. We also proposed an optimal pose control method which method combines the sliding mode control with the optimal control theory in this paper. By introducing an integral compensation term, the optimal regulator is robust and the reaching mode of the sliding mode control is eliminated. This control methods could also eliminate the influence that the big load inertia ratio and the uncertain factors of the air-bearing pose control system had on the control precision. The experimental results indicate that the control accuracy of the system meets the task requirements and the correctness and feasibility of this scheme are verified.
机译:根据中国月球探测计划第三步模拟月球轨道器对接和样品传输过程的地面实验台的要求,设计了一个六自由度的含气模拟平台系统。本文还提出了一种最优姿态控制方法,该方法将滑模控制与最优控制理论相结合。通过引入积分补偿项,最优调节器具有鲁棒性,并且消除了滑模控制的到达模式。该控制方法还可以消除大惯量比和空载姿态控制系统的不确定因素对控制精度的影响。实验结果表明,该系统的控制精度满足任务要求,验证了该方案的正确性和可行性。

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