Robust nonlinear motion control of a helicopter

A. Isidori, L. Marconi, A. Serrani
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引用次数: 295

Abstract

We consider the problem of controlling the vertical motion of a nonlinear model of a helicopter to a reference signal, while stabilizing the lateral and horizontal position and maintaining a constant attitude. The reference to be tracked is given by a sum of a constant and a fixed number of sinusoidal signals, and it is assumed not to be available to the controller. This represents a possible situation in which the helicopter is required to synchronize its vertical motion with that of an oscillating platform, as the one given by a sea carrier subject to wave-induced oscillations. We design a nonlinear controller which combines results on nonlinear adaptive output regulations and robust stabilization of systems in feedforward form by means of saturated controls. Simulation results show the effectiveness of the method and its ability to cope with large uncertainties on the plant, the actuator model and the exogenous reference signal.
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直升机鲁棒非线性运动控制
考虑了将直升机非线性模型的垂直运动控制为参考信号,同时稳定横向和水平位置并保持恒定姿态的问题。要跟踪的参考由一个常数和一个固定数量的正弦信号的和给出,并且假定控制器不可用。这代表了一种可能的情况,在这种情况下,直升机需要与振荡平台的垂直运动同步,就像受波浪引起的振荡影响的海上航母一样。我们设计了一种非线性控制器,它结合了非线性自适应输出调节的结果和采用饱和控制的前馈形式系统的鲁棒镇定。仿真结果表明了该方法的有效性,能够处理被控对象、执行器模型和外源参考信号的较大不确定性。
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Linear symmetry of nonlinear systems On-line predictive techniques for "differentiated services" networks The Lie algebra structure of spin systems and their controllability properties Time-delayed chaos control with repetitive learning Robust nonlinear motion control of a helicopter
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