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Design of hovering altitude holding control system for helicopter

机译:直升机悬停高度保持控制系统设计

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Effected by sea wave and other noises, altitude holding becomes difficult when helicopter is hovering or rescuing near the sea face. In this paper, according to the integrated height system of radio altimeter and vertical accelerometer, a Kalman filter is designed to get the accurate altitude signals of the helicopter hovering over the sea. Then, two altitude holding control structures are developed based on helicopter explicit model following control system (EMFCS), which has excellent operation characteristics. In order to simulate the real situation and to design the filter, sea wave model is established by using the rational spectrum modeling method. Simulation results show that the two control systems designed both can realize helicopter hovering altitude holding efficiently, and have good resistance to vertical wind disturbance or parametric perturbations.
机译:受海浪和其他噪音的影响,当直升机在海面附近徘徊或营救时,很难保持高度。本文根据无线电高度仪和垂直加速度计的集成高度系统,设计了一个卡尔曼滤波器来获取直升机悬停在海上的准确高度信号。然后,基于直升机显式模型跟随控制系统(EMFCS)开发了两种高度保持控制结构,具有良好的运行特性。为了模拟真实情况并设计滤波器,采用合理的频谱建模方法建立了海浪模型。仿真结果表明,所设计的两种控制系统均能有效实现直升机的悬停高度保持,并具有良好的抵抗垂直风扰或参数扰动的能力。

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