Matthieu Jeanneau (auth.), Declan Bates, Martin Hagström (eds.)9783540737186, 3540737189
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 continuous increase in the complexity of aircraft control laws, and the corresponding – crease in the demands on their performance and reliability, industrial control law designers are highly motivated to explore the applicability of new and more powerful methods for design and analysis. The successful application of fully nonlinear control techniques to aircraft control problems o?ers the prospect of improvements in several di?erent areas. Firstly, there is the possibility of – proving design and analysis criteria to more fully re?ect the nonlinear nature of the dynamics of the aircraft. Secondly, the time and e?ort required on the part of designers to meet demanding speci?cations on aircraft performance and h- dling could be reduced. Thirdly, nonlinear analysis techniques could potentially reduce the time and resources required to clear ?ight control laws, and help to bridge the gap between design, analysis and ?nal ?ight clearance. Theaboveconsiderationsmotivatedtheresearchpresentedinthisbook,which is the result of a three-year research e?ort organised by the Group for Aeron- tical Research and Technology in Europe (GARTEUR). In September 2004, GARTEUR Flight Mechanics Action Group 17 (FM-AG17) was established to conduct research on ”New Analysis and Synthesis Techniques for Aircraft Control”. |
Table of contents : Front Matter….Pages I-VIII Front Matter….Pages 1-1 The AIRBUS On-Ground Transport Aircraft Benchmark….Pages 3-24 On-Ground Transport Aircraft Nonlinear Control Design and Analysis Challenges….Pages 25-33 The ADMIRE Benchmark Aircraft Model….Pages 35-54 Nonlinear Flight Control Design and Analysis Challenge….Pages 55-65 Front Matter….Pages 67-67 Nonlinear Symbolic LFT Tools for Modelling, Analysis and Design….Pages 69-92 Nonlinear LFT Modelling for On-Ground Transport Aircraft….Pages 93-115 On-Ground Aircraft Control Design Using an LPV Anti-windup Approach….Pages 117-145 Rapid Prototyping Using Inversion-Based Control and Object-Oriented Modelling….Pages 147-173 Robustness Analysis Versus Mixed LTI/LTV Uncertainties for On-Ground Aircraft….Pages 175-194 Front Matter….Pages 195-195 An LPV Control Law Design and Evaluation for the ADMIRE Model….Pages 197-229 Block Backstepping for Nonlinear Flight Control Law Design….Pages 231-257 Optimisation-Based Flight Control Law Clearance….Pages 259-300 Investigation of the ADMIRE Manoeuvring Capabilities Using Qualitative Methods….Pages 301-324 Front Matter….Pages 325-325 Industrial Evaluation….Pages 327-339 Concluding Remarks….Pages 341-342 Back Matter….Pages 343-360 |
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