Xiangwei Bu;Ruining Luo;Jiaxi Chen;Humin Lei
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引用次数: 0

摘要

我们的目标是为受饱和约束动力学影响的离散时间系统,特别是无人机飞行控制领域,探索一种具有脆性抑制功能的有限时间跟踪控制协议。该协议能够对跟踪误差施加所需的瞬态和稳态行为,同时利用有限时间性能函数引入转换误差,并通过在类似后步法的控制设计中使用这些函数开发的反馈项间接稳定误差。我们的方法引入了一种结构,使其有别于现有的基于转换误差稳定的规定性能控制(PPC)方法。此外,我们还提出了一种补偿系统来修改最终反馈项并解决执行器饱和问题,从而有效解决了与现有 PPC 方法相关的具有挑战性的脆弱性问题,该问题是由离散时间系统中执行器饱和导致的误差波动引起的。最后,在飞行控制应用中获得的比较仿真结果验证了我们设计的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fragility-Rejection UAV Flight Control With Discrete-Time Constrained Dynamics Endowing Preselected Qualities
Our objective is to explore a finite-time tracking control protocol with fragility-rejection for discrete-time systems subject to saturation constrained dynamics, specifically in the field of UAV flight control. This protocol is capable of imposing desired transient and steady-state behaviors on tracking errors, while introducing transformed errors utilizing finite-time performance functions and stabilizing them indirectly through feedback terms developed using these functions in a back-stepping-like control design. Our approach introduces a structure that distinguishes it from existing transformed-error-stabilization-based prescribed performance control (PPC) methods. Furthermore, we propose a compensated system to modify the final feedback term and address actuator saturation, effectively resolving the challenging fragility issue associated with existing PPC approaches caused by error fluctuation due to actuator saturation in discrete-time systems. Finally, comparative simulation results obtained for flight control applications validate the effectiveness of our design.
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