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An adaptive compensation strategy of control surfaces free-play

机译:控制面自由运动的自适应补偿策略

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A technique aimed to neutralize the presence of free-play effects in a control surface actuation chain is presented. The procedure is based on the inversion of a function approximating such a nonlinearity. A simple yet robust on-line adaptive algorithm is proposed to identify the free-play parameters, i.e. free-play width and the equivalent control stiffness. To achieve such a compensation, the only measures required are those of the control surface deflection and the hinge torque. The procedure is then coupled with an other adaptive control law to drastically reduce possible residual limit cycle oscillations in closed loop associated to the free-play presence. Within such a framework, the proposed compensation can be interpreted as a control augmentation which can be easily extended to multiple control surfaces. Even if only numerical analyses are considered in this work, measurement noise is taken into account, and both free-play and friction are simulated in the control surface actuation system, aiming to increase the reliability of the presented results. In addition, several off-design conditions are analyzed, e.g. varying the free-play width and friction amplitude. The proposed methodology is applied to a three degrees of freedom airfoil in transonic regime. This case is characterized by highly nonlinear unsteady aerodynamic loads, producing significant shock motions and large limit cycle oscillations at a relatively high frequency, resulting so in a challenging test for the proposed approach.
机译:提出了一种旨在中和控制面驱动链中自由运动效应的技术。该过程基于近似于这种非线性的函数的求逆。提出了一种简单而健壮的在线自适应算法来识别自由运动参数,即自由运动宽度和等效控制刚度。为了实现这种补偿,所需的唯一措施是控制表面挠度和铰链扭矩。然后,该过程与其他自适应控制定律相结合,以大幅度减少与自由活动相关的闭环中可能出现的剩余极限循环振荡。在这样的框架内,建议的补偿可以解释为一种控制扩展,可以很容易地扩展到多个控制表面。即使在这项工作中仅考虑数值分析,也要考虑到测量噪声,并在控制面驱动系统中模拟自由游隙和摩擦,以提高所提出结果的可靠性。此外,还分析了几种非设计条件,例如改变自由运动的宽度和摩擦幅度。所提出的方法应用于跨音速状态的三自由度翼型。这种情况的特征是高度非线性的非稳态气动载荷,在相对较高的频率下产生明显的冲击运动和较大的极限循环振荡,因此对所提出的方法进行了具有挑战性的测试。

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