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Robust linear PID controller for satellite attitude stabilisation and attitude tracking control

机译:用于卫星姿态稳定和姿态跟踪控制的鲁棒线性PID控制器

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摘要

In this paper, a linear robust PID controller is presented for satellite attitude stabilisation and attitude tracking control. The PID controller presented in this paper has the advantage that: 1) the Lyapunov function is modified thus the stability of the system is easier to prove; 2) the constraints of the parameters are broadened thus parameters are easier to choose comparing with existing methods; 3) the controller is robust to bounded disturbance torque and the satellite inertia matrix; 4) the controller is linear thus it is convenient for practical application. The proof of the stability and the constraints of the parameters are given in this paper. The simulation results verify the feasibility of the controller presented in this paper.
机译:本文提出了一种线性鲁棒PID控制器,用于卫星姿态稳定和姿态跟踪控制。本文提出的PID控制器具有以下优点:1)修改了Lyapunov函数,从而更易于证明系统的稳定性; 2)拓宽了参数约束条件,与现有方法相比,参数更易于选择; 3)控制器对有界干扰转矩和卫星惯性矩阵具有鲁棒性; 4)控制器是线性的,因此便于实际应用。给出了稳定性和参数约束的证明。仿真结果验证了本文提出的控制器的可行性。

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