Optimization Problems for Aircraft Flight in a Windshear View Full Text


Ontology type: schema:Chapter     


Chapter Info

DATE

1989

AUTHORS

A. Miele , T. Wang

ABSTRACT

This chapter presents an overview of the optimization problems having interest for the flight of an aircraft in a windshear. Three problems are studied: (P1) for take-off trajectories, the minimization of the maximum deviation of the absolute path inclination from a reference value; here, relative path inclination recovery is required at the final point; (P2) for abort landing trajectories, the minimization of the maximum drop of altitude from a reference value; here, the transition from descending flight to ascending flight is required; (P3) for penetration landing trajectories, the minimization of a performance index measuring the deviation of the flight trajectory from the nominal trajectory; here, the touchdown path inclination is specified and the values of the trouchdown distance and the touchdown velocity must be in a specified range. Problems (P1) and (P2) are Chebyshev problems of optimal control, and Problem (P3) is a Bolza problem of optimal control. These problems are solved by means of the sequential gradient-restoration algorithm for optimal control problems. More... »

PAGES

277-305

Book

TITLE

Nonsmooth Optimization and Related Topics

ISBN

978-1-4757-6021-7
978-1-4757-6019-4

Identifiers

URI

http://scigraph.springernature.com/pub.10.1007/978-1-4757-6019-4_17

DOI

http://dx.doi.org/10.1007/978-1-4757-6019-4_17

DIMENSIONS

https://app.dimensions.ai/details/publication/pub.1051511161


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