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Trajectory Optimization and Guidance for a HERMES-Type Reentry Vehicle

Jänsch, C. and Markl, A. (1991) Trajectory Optimization and Guidance for a HERMES-Type Reentry Vehicle. In: Proc. AIAA-91-2659-CP, Vol.1/3, pp. 543-553. AIAA, The Aerospace Center, Washington DC. AIAA Guidance Navigation & Control Conference, New Orleans, 12.-14.08.91.

Full text not available from this repository.

Abstract

The paper presents a guidance scheme and several optimal reentry trajectories for a HERMES type reentry vehicle from a low-earth orbit mission to a landing site in Southern France. The guidance scheme is an extension of the guidance principles employed by the U.S. Space Shuttle. In particular, the range-control by linearization is replaced by an on-line optimization using the full nonlinear dynamics with a low parameterization for the velocity dependent drag-profile.

Item URL in elib:https://elib.dlr.de/27845/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1991,
Title:Trajectory Optimization and Guidance for a HERMES-Type Reentry Vehicle
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Jänsch, C.UNSPECIFIEDUNSPECIFIED
Markl, A.UNSPECIFIEDUNSPECIFIED
Date:1991
Journal or Publication Title:Proc. AIAA-91-2659-CP
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol.1/3
Page Range:pp. 543-553
Publisher:AIAA, The Aerospace Center, Washington DC
Status:Published
Keywords:HERMES type reentry vehicle; Thermal Protection System (TPS);
Event Title:AIAA Guidance Navigation & Control Conference, New Orleans, 12.-14.08.91
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Robotics and Mechatronics (until 2012) > Institut für Dynamik der Flugsysteme
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 06:47

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