Trajectory reconfiguration for an unmanned aircraft

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

doi:10.2514/6.2002-4674

Trajectory reconfiguration for an unmanned aircraft

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

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

7 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 language	English (US)
Title of host publication	AIAA Guidance, Navigation, and Control Conference and Exhibit
Publisher	American Institute of Aeronautics and Astronautics [email protected]
ISBN (Print)	9781563479786
DOIs	https://doi.org/10.2514/6.2002-4674
State	Published - Jan 1 2002
Externally published	Yes

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Generated from Scopus record by KAUST IRTS on 2021-02-18

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10.2514/6.2002-4674

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title = "Trajectory reconfiguration for an unmanned aircraft",

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. {\textcopyright} 2002 by the author(s). Published by the American Institute of Aeronautics and Astronautics, Inc.",

author = "M. Valenti and B. Mettler and T. Schouwenaars and E. Feron and J. Paduano",

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year = "2002",

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AU - Valenti, M.

AU - Mettler, B.

AU - Schouwenaars, T.

AU - Feron, E.

AU - Paduano, J.

N1 - Generated from Scopus record by KAUST IRTS on 2021-02-18

PY - 2002/1/1

Y1 - 2002/1/1

N2 - 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.

AB - 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.

UR - http://arc.aiaa.org/doi/10.2514/6.2002-4674

UR - http://www.scopus.com/inward/record.url?scp=85087595338&partnerID=8YFLogxK

U2 - 10.2514/6.2002-4674

DO - 10.2514/6.2002-4674

M3 - Conference contribution

SN - 9781563479786

BT - AIAA Guidance, Navigation, and Control Conference and Exhibit

PB - American Institute of Aeronautics and Astronautics [email protected]

ER -

Trajectory reconfiguration for an unmanned aircraft

Abstract

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