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Inverse optimal controller design for a quadrotor unmanned aerial vehicle

机译:四旋翼无人机的逆最优控制器设计

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This paper presents the application of inverse optimal control approach to an unmanned quadrotor air vehicle system. Here, the inverse optimal controller is designed to solve the reference tracking problem relying on the use of control Lyapunov function. In the establishment of the control law, the affine-in-input discrete-time nonlinear system model is taken into consideration. A stabilizing feedback control law is constructed such that control Lyapunov function is known a priori. After stability examination and determination of a meaningful cost functional, respective cost functional is optimized. Then, a matrix that minimizes a tracking error function is searched using PSO algorithm. The designed controller has been applied to a nonlinear model of a quadrotor. It is shown that the proposed controller guarantees a fast convergence and makes the quadrotor stabilize itself very fast and follow aggressive trajectories accurately under certain circumstances.
机译:本文提出了逆最优控制方法在无人四旋翼飞行器系统中的应用。这里,逆最优控制器被设计为依靠控制李雅普诺夫函数的使用来解决参考跟踪问题。在建立控制律时,考虑了仿射输入离散时间非线性系统模型。构造稳定的反馈控制定律,使得先验已知控制李雅普诺夫函数。在稳定性检查和确定有意义的成本函数之后,对各个成本函数进行优化。然后,使用PSO算法搜索最小化跟踪误差函数的矩阵。设计的控制器已应用于四旋翼的非线性模型。结果表明,所提出的控制器保证了快速收敛,并使四旋翼非常快速地稳定自身,并在某些情况下准确地遵循了侵略性的轨迹。

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