Nonlinear Analysis and Synthesis Techniques for Aircraft Control
Despite many signi?cant advances in the theory of nonlinear control in recent years, the majority of control laws implemented in the European aerospace - dustry are still designed and analysed using predominantly linear techniques applied to linearised models of the aircrafts dynamics. Given the con...
محفوظ في:
| المؤلف الرئيسي: | |
|---|---|
| مؤلفون آخرون: | |
| التنسيق: | Livre numérique |
| اللغة: | Anglais |
| منشور في: |
Berlin, Heidelberg :
Springer Berlin Heidelberg
[20..].
Cham : Springer Nature |
| الطبعة: | 1st ed. 2007. |
| سلاسل: | Lecture Notes in Control and Information Sciences
365 |
| الموضوعات: | |
| الوصول للمادة أونلاين: | Accès sur la plateforme de l'éditeur Accès sur la plateforme Istex Accès Université d'Orléans Accès INSA CVL |
| ملاحظة: |
Archives Springer e-books (Licence nationale) Archives Springer e-books (Licence nationale) |
| Autres localisations: | Voir dans le Sudoc |
| Edition sous un autre format: | • Nonlinear analysis and synthesis techniques for aircraft control, Declan Bates, Martin Hagström, éd., Berlin, Springer, 2007, 1 vol. (VIII-360 p.), Lecture notes in control and information sciences, 3-540-73718-9 |
جدول المحتويات:
- Benchmarks and Design and Analysis Challenges The AIRBUS On-Ground Transport Aircraft Benchmark On-Ground Transport Aircraft Nonlinear Control Design and Analysis Challenges The ADMIRE Benchmark Aircraft Model Nonlinear Flight Control Design and Analysis Challenge Applications to the Airbus Benchmark Nonlinear Symbolic LFT Tools for Modelling, Analysis and Design Nonlinear LFT Modelling for On-Ground Transport Aircraft On-Ground Aircraft Control Design Using an LPV Anti-windup Approach Rapid Prototyping Using Inversion-Based Control and Object-Oriented Modelling Robustness Analysis Versus Mixed LTI/LTV Uncertainties for On-Ground Aircraft Applications to the ADMIRE Benchmark An LPV Control Law Design and Evaluation for the ADMIRE Model Block Backstepping for Nonlinear Flight Control Law Design Optimisation-Based Flight Control Law Clearance Investigation of the ADMIRE Manoeuvring Capabilities Using Qualitative Methods Industrial Evaluation and Concluding Remarks Industrial Evaluation Concluding Remarks