Bi-objective pseudospectral optimal control techniques for aircraft trajectory optimisation
conference contribution
posted on 2024-10-31, 17:15 authored by Kenneth Chircop, David Zammit-Mangion, Roberto SabatiniRoberto SabatiniThe paper presents the optimal control techniques used to perform bi-objective flight trajectory optimization. Direct methods are applied in conjunction with the adaptive bisection epsilon-constraint scalarization method, and a generic A320 airliner model, to generate pareto frontiers for climb trajectories optimized for minimum time and fuel.
History
Start page
3546End page
3555Total pages
10Outlet
Proceedings of the 28th International Congress of the Aeronautical SciencesEditors
Professor I GrantName of conference
ICAS 2012Publisher
International Council of the Aeronautical SciencePlace published
Bonn, GermanyStart date
2012-09-23End date
2012-09-28Language
EnglishCopyright
© 2012 International Council of the Aeronautical Science, AuthorsFormer Identifier
2006043024Esploro creation date
2020-06-22Fedora creation date
2015-01-20Usage metrics
Categories
- Aircraft performance and flight control systems
- Avionics
- Aerospace engineering not elsewhere classified
- Automation engineering
- Navigation and position fixing
- Engineering instrumentation
- Calculus of variations, mathematical aspects of systems theory and control theory
- Applied mathematics not elsewhere classified
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