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Methodologie pour le controle longitudinal d'un avion avec contraintes de qualites de manoeuvrabilite (French text).

机译:具有可操纵性质量约束的飞机的纵向控制方法(法文)。

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A methodology is given in order to choose the gains of two longitudinal flight controls of a Bombardier Inc. aircraft while satisfying the handling qualities fixed by the manufacturer.; The first part of this project consists in analyzing the data and the two flight controls. Then a simple presentation of the handling qualities is made to familiarize the reader with them. Finally, a short introduction to the Guardians Maps is presented: they are scalar maps of gains or uncertain parameters that allow us to find set of values that place poles of our system within a region of the complex plane.; The second part is dedicated to the proposed guidelines. We explain first how to reduce our system to use more efficiently the Guardian Maps. Then we determine the gains that ensure a certain damping for some of the poles. Other handling qualities are fixed by another method. A graphical user interface makes things easier to use the methodology and to view instantly the results for given gains.; The research is closed by an extension of the methodology in order to make Gain Scheduling and to synthesize a robust controller against mass and/or center of gravity variations.
机译:给出了一种方法,以选择庞巴迪公司飞机的两个纵向飞行控制装置的收益,同时满足制造商确定的处理质量。该项目的第一部分包括分析数据和两个飞行控制。然后对处理质量进行简单介绍,以使读者熟悉它们。最后,简要介绍了监护人地图:它们是增益或不确定参数的标量地图,使我们能够找到一组将系统极点置于复杂平面区域内的值。第二部分致力于拟议的准则。我们首先说明如何减少我们的系统以更有效地使用Guardian Maps。然后,我们确定可确保某些极点具有一定阻尼的增益。其他处理质量是通过其他方法确定的。图形用户界面使使用该方法更容易,并且可以立即查看给定收益的结果。通过扩展方法来结束研究,以便进行增益调度并针对质量和/或重心变化合成鲁棒的控制器。

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