四旋翼鲁棒跟踪:一种连续滑模控制策略

Romeo Falcón, Oscar A. Gonzalez, H. Ríos, A. Dzul
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引用次数: 2

摘要

四旋翼飞行器的鲁棒跟踪控制设计是当前一个重要而富有挑战性的问题。针对外部扰动和不确定性影响下的四旋翼,提出了一种鲁棒跟踪输出控制策略。该策略由有限时间滑模观测器(FT-SMO)组成,该观测器从可测输出中估计完整状态并识别某些类型的干扰;以及PID控制器和连续滑模控制器(Continuous- smc)之间的组合,该控制器可以指数鲁棒地跟踪期望的时变轨迹,并且不受外部干扰和不确定性的影响。闭环稳定性是基于输入状态稳定性(ISS)和有限时间稳定性(FT-ISS)特性提供的。最后,一些实时实验结果验证了所提控制策略的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Quad-Rotor Robust Tracking: A Continuous Sliding-Mode Control Strategy
The design of robust tracking control for Quad-Rotors is an important and challenging problem nowadays. In this paper a robust tracking output-control strategy is proposed for a Quad-Rotor under the influence of external disturbances and uncertainties. Such a strategy is composed of a Finite-Time Sliding-Mode Observer (FT-SMO) which estimates the full state from the measurable output and identifies some type of disturbances; and also of a combination between PID controllers and a Continuous Sliding-Modes Controller (Continuous-SMC), that exponentially robustly track a desired time-varying trajectory and despite the influence of external disturbances and uncertainties. The closed-loop stability is provided based on Input-to-State Stability (ISS) and Finite-Time ISS (FT-ISS) properties. Finally, some experimental results in real-time show the performance of the proposed control strategy.
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