Titlebook: Advanced Techniques for Clearance of Flight Control Laws; Christopher Fielding,Andras Varga,Michiel Selier Book 2002 Springer-Verlag Berli

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Robert E. Kearney,Robert F. Kirschich “anti”-optimisation is performed to determine the worst-case parameter combination/flight condition leading to worst performance. The basic requirements for the applicability of the optimisation-based approach are the availability of suitable parametric models describing the overall nonlinear dy

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Nikolai Aleksandrovich Bernsteinere clearance criteria have to be checked are defined. The uncertainty parameters to be considered for the analysis are listed and categorised. Finally, each clearance criterion selected for the HIRM+ is described and mathematically defined.

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https://doi.org/10.1007/978-3-642-17177-2d LFT in order to clear critical areas in the flight envelope. .-Analysis allows to determine the combination of uncertain parameters within their respective bounds, for which a performance criterion or stability margin is worst. For a sensible worst-case analysis, it is important that the uncertain

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https://doi.org/10.1007/978-3-642-32603-5trajectory is given. Five of the most relevant uncertainties on the pitch axis are considered. This model describes the gap along a trajectory passing through flight condition FC1, with an angle of attack equal to 6°. The proposed approach is based on a simplified longitudinal model used to determin

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Biomechanics in Medicine and Biologygitudinal and lateral flight dynamics. Of the five clearance criteria specified for investigation in Chapter 10, we address the Stability Margin and Unstable Eigenvalue criteria in detail. Comments on the applicability of .-analysis to the other criteria are included at the end of the chapter.