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Integrator Back-Stepping Algorithm on Attitude Control of Quadrotor Helicopter Based on Disturbance Observer

机译:基于干扰观察者的四轮车直升机姿态控制积分器回踏步算法

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摘要

When quadrotor helicopter was in the process of attitude control, it would often have the serious problem of external interference. So disturbance observer was designed to realize real-time estimation of disturbing moment. In this case, adaptive regime is introduced to the law of integrator back-Stepping control. And experiments were made to verify the algorithm. The experiments show that the algorithm could cope with a certain range of external disturbance, and made significant improve in its accuracy and robustness.
机译:当Quadrotor直升机处于态度控制过程中,它通常会有外部干扰的严重问题。因此,扰动观察者旨在实现令人不安的时刻的实时估计。在这种情况下,将自适应制度引入积分器后台控制的定律。并进行实验以验证算法。实验表明,该算法可以应对一定范围的外部干扰,并在其准确性和稳健性方面取得了重大改善。

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