DocumentCode :
2066713
Title :
Footprint calculation methods for a reusable launch vehicle
Author :
Ngo, Anhtuan D. ; Doman, David B.
Author_Institution :
U. S. Air Force Res. Lab., Wright-Patterson AFB, OH, USA
Volume :
3
fYear :
2002
fDate :
2002
Firstpage :
1930
Abstract :
An important element of an adaptive and reconfigurable guidance and control system is the ability to compute the largest area (footprint) on the earth´s surface that is reachable by the autonomous vehicle under the current operating condition. During an abort situation when it suddenly becomes necessary to divert the vehicle from its original landing site, the knowledge of this reachable area can assist in choosing a safe and available landing site. In the paper, a technique based on calculus of variations is applied to find the footprint of an autonomous vehicle subject to operating constraints.
Keywords :
adaptive control; aerospace control; space vehicles; variational techniques; abort situation; adaptive reconfigurable guidance and control system; autonomous vehicle; calculus of variations; footprint calculation methods; operating constraints; reachable area; reusable launch vehicle; Actuators; Adaptive control; Control systems; Mobile robots; Navigation; Propulsion; Remotely operated vehicles; Space vehicles; Trajectory; Vehicle safety;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2002. Proceedings of the 2002
ISSN :
0743-1619
Print_ISBN :
0-7803-7298-0
Type :
conf
DOI :
10.1109/ACC.2002.1023917
Filename :
1023917
Link To Document :
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