Optimization of the tether-assisted return mission of a guided re-entry capsule-Reference-Cited by-同舟云学术

Optimization of the tether-assisted return mission of a guided re-entry capsule

Published:2005-11 Issue:8 Volume:9 Page:713-721
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zimmermann Frank,Schöttle Ulrich M.,Messerschmid Ernst

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference21 articles.

1. Y.N. Andrés, F. Zimmermann, U.M. Schöttle, Optimization and control of the early deployment phase during a tether-assisted deorbit maneuver, in: Proceedings of the 22nd International Symposium on Space Technology and Science, ISTS 2000-k-22v, Morioka, Japan, May 28–June 4, 2000

2. Optimal control of the shuttle-tethered-subsatellite system;Bainum;Acta Astronautica,1980

3. J. Burkhardt, Konzeptioneller Systementwurf und Missionsanalyse für einen auftriebsgestützten Rückkehrkörper, Dissertation, Universität Stuttgart, 2001

4. Operational use of guided reentry capsules – system design solutions and mission safety considerations;Burkhardt;Aerospace Science and Technology,2004

5. F. Farachi, F. Zimmermann, U.M. Schöttle, Impact of a tether-assisted deorbitation on the performance of guided capsule re-entry, in: Deutscher Luft- und Raumfahrtkongreß 1999, DGLR-JT99-203, Berlin, September 1999

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