Extending Flat Motion Planning to Non-flat Systems. Experiments on Aircraft Models Using Maple

F. Ollivier
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引用次数: 3

Abstract

Aircraft models may be considered as flat if one neglects some terms associated to aerodynamics. Computational experiments in Maple show that in some cases a suitably designed feed-back allows to follow such trajectories, when applied to the non-flat model. However some maneuvers may be hard or even impossible to achieve with this flat approximation. In this paper, we propose an iterated process to compute a more achievable trajectory, starting from the flat reference trajectory. More precisely, the unknown neglected terms in the flat model are iteratively re-evaluated using the values obtained at the previous step. This process may be interpreted as a new trajectory parametrization, using an infinite number of derivatives, a property that may be called generalized flatness. We illustrate the pertinence of this approach in flight conditions of increasing difficulties, from single engine flight, to aileron roll.
将平面运动规划扩展到非平面系统。用Maple制作飞机模型的实验
如果忽略与空气动力学有关的一些术语,飞机模型可能被认为是平坦的。Maple的计算实验表明,在某些情况下,当应用于非平面模型时,适当设计的反馈允许遵循这样的轨迹。然而,有些机动可能很难甚至不可能实现这种平近似。在本文中,我们提出了一个迭代过程来计算一个更容易实现的轨迹,从平坦的参考轨迹开始。更准确地说,平面模型中被忽略的未知项使用前一步获得的值进行迭代重新评估。这个过程可以被解释为一种新的轨迹参数化,它使用了无穷多的导数,这种性质可以被称为广义平坦性。我们说明了这种方法在日益困难的飞行条件下的针对性,从单引擎飞行到副翼滚转。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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