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

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樓主: indulge
51#
發(fā)表于 2025-3-30 11:05:01 | 只看該作者
52#
發(fā)表于 2025-3-30 15:13:09 | 只看該作者
https://doi.org/10.1007/978-3-642-17177-2l is generated and compared with one obtained using an affine modelling approach. Although both model representations are aimed to cover the same flight conditions, the affine model is a function of a large number of artificial parameters. Both models are compared regarding their ease of generation, conservatism, accuracy, and applicability.
53#
發(fā)表于 2025-3-30 17:32:51 | 只看該作者
54#
發(fā)表于 2025-3-30 23:22:40 | 只看該作者
55#
發(fā)表于 2025-3-31 02:40:46 | 只看該作者
Book 2002 Control Laws are presented as well as classical and particularly new analysis methods. The different methods are evaluated and compared and their potential application to Civil Aircraft is demonstrated.
56#
發(fā)表于 2025-3-31 06:14:18 | 只看該作者
Jack M. Winters,Patrick E. Cragomodel is described as one of the benchmark military aircraft models used within FM(AG-11). HIRM+ originates from the HIRM (High Incidence Research Model) developed within the GARTEUR Action Group on Robust Flight Control FM(AG-08). In building the HIRM+, additional emphasis has been put on realistic modelling of parametric uncertainties.
57#
發(fā)表于 2025-3-31 09:43:22 | 只看該作者
https://doi.org/10.1007/978-3-642-32603-5 state-space trajectory. First the LFT generation by flatness approach is described. Then an LFT model of the open loop HIRM+ model for the above flight condition is given. Thereafter an LFT model of the closed loop HIRM+RIDE is proposed to allow the identification of worst case stability margin.
58#
發(fā)表于 2025-3-31 15:49:17 | 只看該作者
Tasks and Needs of the Industrial Clearance Process978-3-030-75859-2
59#
發(fā)表于 2025-3-31 20:13:04 | 只看該作者
60#
發(fā)表于 2025-3-31 23:38:22 | 只看該作者
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