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