H∞ for quadrotor attitude stabilization

Wesam M. Jasim, Dongbing Gu
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引用次数: 13

Abstract

This paper proposes a state feedback controller for the attitude stabilization problem of quadrotors. The quadrotor attitude is represented by unit quaternion and disturbance of the attitude model is taken into consideration. A robust controller is synthesized via H∞ optimal design approach. Solving the nonlinear H∞ optimal control problem using state feedback is meltdown to finding a solution to a Hamilton-Jacobi inequality. Based on the quadrotor attitude dynamics, an appropriate parameterized Lyapunov function is selected and the corresponding state feedback controller is derived. Then the parameters are found from a Hamilton-Jacobi inequality. The resultant state feedback controller can lead to closed-loop nonlinear system having L2-gain less than or equal to a constant γ, and establish the asymptotically stability of the closed-loop nonlinear system without external disturbance. The simulation provides the results to show the stability and the robust performance against to disturbance.
H∞用于四旋翼姿态稳定
针对四旋翼机姿态稳定问题,提出了一种状态反馈控制器。采用单位四元数表示四旋翼姿态,并考虑姿态模型的扰动。采用H∞优化设计方法合成了鲁棒控制器。利用状态反馈求解非线性H∞最优控制问题就是求解Hamilton-Jacobi不等式。基于四旋翼姿态动力学,选择合适的参数化Lyapunov函数,推导出相应的状态反馈控制器。然后根据Hamilton-Jacobi不等式求出参数。所得到的状态反馈控制器可以使闭环非线性系统的l2增益小于或等于常数γ,并建立无外部干扰的闭环非线性系统的渐近稳定性。仿真结果表明,该系统具有良好的稳定性和抗干扰的鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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