Trajectory reconfiguration for an unmanned aircraft

M. Valenti, B. Mettler, T. Schouwenaars, E. Feron, J. Paduano

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Scopus citations

Abstract

We investigate strategies for guidance-level reconfiguration following changes in aircraft closed-loop dynamics. The guidance model for the vehicle under study is a maneuver automaton. We propose reconfiguration methods to handle changes in such vehicle dynamics using the Guidance Value Function that emerges from the solution to the underlying optimal trajectory generation problem. We illustrate our approach on a numerical example. © 2002 by the author(s). Published by the American Institute of Aeronautics and Astronautics, Inc.
Original languageEnglish (US)
Title of host publicationAIAA Guidance, Navigation, and Control Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc.custserv@aiaa.org
ISBN (Print)9781563479786
DOIs
StatePublished - Jan 1 2002
Externally publishedYes

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