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Passivity-based simple adaptive control for quadrotor helicopter in the presence of actuator dynamics

机译:存在执行器动力学的基于被动性的四旋翼直升机简单自适应控制

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In this paper, a passivity-based simple adaptive control strategy is proposed for the attitude and altitude control of Quadrotor Helicopter in the presence of actuator dynamics. The proposed adaptive control requires the system to be Almost Strictly Passive (ASP) or Almost Strictly Positive Real (ASPR) in linear time-invariant (LTI) systems so that the closed-loop stability can be guaranteed. Unfortunately, most of systems in the real world including Quadrotors do not satisfy the ASP/ASPR conditions and especially in the presence of actuator dynamics. To this effect, the so-called Parallel Feedforward Compensator (PFC) is introduced to achieve the required conditions. Stability of the closed-loop adaptive system is established. The efficiency and high performance of the proposed adaptive controller are verified through simulation for the Quadrotor Helicopter.
机译:本文提出了一种基于无源性的简单自适应控制策略,在执行器动力学存在的情况下,对四旋翼直升机的姿态和高度进行控制。所提出的自适应控制要求系统在线性时不变(LTI)系统中为几乎严格无源(ASP)或几乎完全为正实数(ASPR),以便可以确保闭环稳定性。不幸的是,现实世界中的大多数系统(包括Quadrotor)都无法满足ASP / ASPR条件,尤其是在执行器动力学存在的情况下。为此,引入了所谓的并联前馈补偿器(PFC)以达到所需条件。建立了闭环自适应系统的稳定性。通过对四旋翼直升机的仿真,验证了所提出的自适应控制器的效率和高性能。

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