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Attitude tracking of mars entry vehicles via fuzzy sampled-data control approach

机译:基于模糊采样数据控制方法的火星进入车辆姿态跟踪

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In this paper, a fuzzy sampled-data attitude tracking controller is designed for Mars entry vehicles. Initially, to reduce the complexity of fuzzy modeling, the original nonlinear attitude system is divided into two subsystems by using two time-scale decomposition method. Subsequently, the dynamic inversion control technique is applied to the slow subsystem to generate the angular velocity command. Then, based on the Takagi-Sugeno (T-S) fuzzy model of the fast subsystem and the angular velocity command, the fuzzy sampled-data controller is designed for the fuzzy tracking error system to derive the desired control torques by using a time-dependent Lyapunov functional. Finally, the simulation results on the Mars entry vehicles are given to illustrate the feasibility and effectiveness of the proposed method.
机译:本文针对火星进入飞行器设计了模糊采样数据姿态跟踪控制器。最初,为降低模糊建模的复杂性,使用两种时标分解方法将原始的非线性姿态系统分为两个子系统。随后,将动态反演控制技术应用于慢速子系统以生成角速度命令。然后,基于快速子系统的Takagi-Sugeno(TS)模糊模型和角速度命令,为模糊跟踪误差系统设计了模糊采样数据控制器,以使用与时间有关的Lyapunov来导出所需的控制转矩。功能。最后,给出了火星进入飞行器的仿真结果,说明了该方法的可行性和有效性。

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