@inproceedings{7a3e5c11de854935967209c43f0f24ce,
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.",
author = "M. Valenti and B. Mettler and T. Schouwenaars and E. Feron and J. Paduano",
year = "2002",
month = jan,
day = "1",
language = "English (US)",
isbn = "9781624101083",
series = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
note = "AIAA Guidance, Navigation, and Control Conference and Exhibit 2002 ; Conference date: 05-08-2002 Through 08-08-2002",
}