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An experimental study of hierarchical autopilot for untrimmed hingeless helicopters

机译:未修剪无铰链直升机分级自动驾驶仪的实验研究

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Different from previous works that require prior trim conditions on the helicopter, this paper proposes a hierarchical PD controller that is robust in controlling untrimmed and therefore critically unstable helicopters. This controller can yield asymptotic stability of the helicopter in horizontal motion control, which can be proven by the linear stability analysis. And this controller can flawlessly engage with traditional dual loop autopilot by using auto-varying references in an inner stabilizing loop. Moreover, to facilitate the controller design, this paper derives the dynamics of hingeless helicopters with an emphasis on gyroscopic effect. Finally, the stability and superior performance of the proposed controller are empirically demonstrated on an instrumented JR Voyager GSR helicopter.
机译:与以前需要在直升机上进行前修剪条件的工作不同,本文提出了一种分级PD控制器,该控制器在控制未修剪并因此极为不稳定的直升机方面具有鲁棒性。该控制器可以在水平运动控制中产生直升机的渐近稳定性,这可以通过线性稳定性分析来证明。通过在内部稳定回路中使用自动变化的参考,该控制器可以完美地使用传统的双回路自动驾驶仪。此外,为方便控制器设计,本文推导了无铰链直升机的动力学特性,重点是陀螺效应。最后,在装有仪表的JR Voyager GSR直升机上通过经验证明了所提出控制器的稳定性和优越性能。

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