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Titlebook: Nonlinear Analysis and Synthesis Techniques for Aircraft Control; Declan Bates,Martin Hagstr?m Book 2007 Springer-Verlag Berlin Heidelberg

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21#
發(fā)表于 2025-3-25 06:51:15 | 只看該作者
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發(fā)表于 2025-3-25 09:07:58 | 只看該作者
23#
發(fā)表于 2025-3-25 11:44:22 | 只看該作者
Nonlinear Symbolic LFT Tools for Modelling, Analysis and Designbines the natural modularity and clarity of presentation from LFT modelling with the ease of manipulation from symbolic algebra. It results in an exact nonlinear symbolic LFT that represents an ideal starting point to apply subsequent assumptions and simplifications to finally transform the model in
24#
發(fā)表于 2025-3-25 15:59:51 | 只看該作者
Nonlinear LFT Modelling for On-Ground Transport Aircraftdentification approach and a general nonlinear symbolic LFT modelling framework. It is shown how the modelling framework is applicable to derive an exact LFT model of the aircraft-on-ground as well as some simplified design-oriented versions. An important contribution is the proposed force identific
25#
發(fā)表于 2025-3-25 21:49:38 | 只看該作者
26#
發(fā)表于 2025-3-26 01:25:21 | 只看該作者
Rapid Prototyping Using Inversion-Based Control and Object-Oriented Modelling modelling approach allows for automatic generation of regular, static, as well as inverse simulation models. Inverse models form the basis of various commonly used nonlinear controller synthesis methods, such as Feedback Linearisation. The resulting multivariable control laws are easily tuned to me
27#
發(fā)表于 2025-3-26 05:50:51 | 只看該作者
28#
發(fā)表于 2025-3-26 11:05:28 | 只看該作者
An LPV Control Law Design and Evaluation for the ADMIRE Modeltransonic and supersonic regions. The design of the LPV control law is based on the parameter-dependent Lyapunov function approach with gridding of the parameter space. It is demonstrated that by using a linear piece-wise interpolation of the aircraft model the LPV approach allows the design of a co
29#
發(fā)表于 2025-3-26 12:45:06 | 只看該作者
30#
發(fā)表于 2025-3-26 19:36:30 | 只看該作者
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