Details
| Originalsprache | Englisch |
|---|---|
| Seiten (von - bis) | 45-69 |
| Seitenumfang | 25 |
| Fachzeitschrift | Optimal Control Applications and Methods |
| Jahrgang | 17 |
| Ausgabenummer | 1 |
| Publikationsstatus | Veröffentlicht - 1996 |
Abstract
This paper presents a numerical investigation of an optimal re-entry manoeuvre under several control and control-state constraints. The essential aim of the optimization is the minimization of the maximal skin temperature of an orbiter. It is demonstrated that the interaction of different solution techniques is indispensable in order to successfully treat such a highly constrained problem. The reduction of the skin temperature is significant. Moreover, the maximum heat flux and the integrated heat flux are also reduced considerably by the optimization.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Steuerungs- und Systemtechnik
- Informatik (insg.)
- Software
- Mathematik (insg.)
- Steuerung und Optimierung
- Mathematik (insg.)
- Angewandte Mathematik
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in: Optimal Control Applications and Methods, Jahrgang 17, Nr. 1, 1996, S. 45-69.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - Mimmizing the maximum heating of a re-entering space shuttle
T2 - An optimal control problem with multiple control constraints
AU - Kreim, H.
AU - Kugelmann, B.
AU - Pesch, H. J.
AU - Breitner, M. H.
N1 - Copyright: Copyright 2018 Elsevier B.V., All rights reserved.
PY - 1996
Y1 - 1996
N2 - This paper presents a numerical investigation of an optimal re-entry manoeuvre under several control and control-state constraints. The essential aim of the optimization is the minimization of the maximal skin temperature of an orbiter. It is demonstrated that the interaction of different solution techniques is indispensable in order to successfully treat such a highly constrained problem. The reduction of the skin temperature is significant. Moreover, the maximum heat flux and the integrated heat flux are also reduced considerably by the optimization.
AB - This paper presents a numerical investigation of an optimal re-entry manoeuvre under several control and control-state constraints. The essential aim of the optimization is the minimization of the maximal skin temperature of an orbiter. It is demonstrated that the interaction of different solution techniques is indispensable in order to successfully treat such a highly constrained problem. The reduction of the skin temperature is significant. Moreover, the maximum heat flux and the integrated heat flux are also reduced considerably by the optimization.
KW - Direct collocation
KW - Minimax optimal control problems
KW - Multiple control-state constraints
KW - Multiple shooting
UR - http://www.scopus.com/inward/record.url?scp=0029772728&partnerID=8YFLogxK
U2 - 10.1002/(SICI)1099-1514(199601/03)17:1<45::AID-OCA564>3.0.CO;2-X
DO - 10.1002/(SICI)1099-1514(199601/03)17:1<45::AID-OCA564>3.0.CO;2-X
M3 - Article
AN - SCOPUS:0029772728
VL - 17
SP - 45
EP - 69
JO - Optimal Control Applications and Methods
JF - Optimal Control Applications and Methods
SN - 0143-2087
IS - 1
ER -