Optimization based clearance of flight control laws a civil aircraft application
.PUBLICATION, DISTRIBUTION, ETC
Place of Publication, Distribution, etc.
Berlin ;New York
Name of Publisher, Distributor, etc.
Springer
Date of Publication, Distribution, etc.
2012
PHYSICAL DESCRIPTION
Specific Material Designation and Extent of Item
xxiv, 449 p. , ill. )some col.( , 24 cm.
SERIES
Series Title
Lecture notes in control and information sciences ;614
GENERAL NOTES
Text of Note
Includes bibliographical references and index.
CONTENTS NOTE
Text of Note
Introduction -- Clearance benchmark for a civil aircraft -- Generation of LPV models and LFRs for a nonlinear aircraft model -- Generation of LFRs for a flexible aircraft model -- Generation of LFRs for a nonlinear controller and closed-loop aircraft models -- Identification of LPV state-space models using H2-minimisation -- Enhanced ]mu[-analysis techniques for clearance -- Worst-case parameter search based clearance using parallel nonlinear programming methods -- Lyapunov-based robustness analysis techniques for clearance -- IQC-based analysis techniques for clearance -- Nonlinear programming methods for worst-case pilot input determination -- Application of ]mu[-analysis techniques to clearance -- Application of parallel nonlinear programming methods for worst-case parameter search -- Applications of Lyapunov-based analysis techniques for clearance -- Applications of IQC-based analysis techniques for clearance - Application of nonlinear programming methods for determination of worst-case pilot inputs -- Evaluation of clearance techniques in an industrial context -- Concluding remarks and industrial perspective -- Assessment of aircraft flight controllers using nonlinear robustness analysis techniques -- Validation and verification )V&V( of safety-critical systems operating under off-nominal conditions -- Clearance of flight control laws for carefree handling of advanced fighter aircraft.
TOPICAL NAME USED AS SUBJECT
Entry Element
، Flight control, Mathematical models
Entry Element
، Airplanes, Control systems
Entry Element
، Airplanes, Evaluation, Mathematics
Entry Element
، Mathematical optimization
DEWEY DECIMAL CLASSIFICATION
Number
629
.
1326015118
LIBRARY OF CONGRESS CLASSIFICATION
Class number
TL
678
.
O6
2012
PERSONAL NAME - PRIMARY RESPONSIBILITY
Relator Code
TI
Entry Element
Andreas Varga, Anders Hansson, and Guilhem Puyou, )eds.(