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Attitude Control Simulation for Equator-S using Object Oriented Modeling

Enderle, W. and Feucht, U. and Moormann, D. (1996) Attitude Control Simulation for Equator-S using Object Oriented Modeling. In: Proceedings 3rd ESA International Conference on Spacecraft Guidance, Navigation and Control Systems. 3rd ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, ESA-ESTEC, Noordwijk, 26.28.11.1996.

Full text not available from this repository.

Abstract

This paper describes efforts for simulation of the Equator-S spacecraft for mission analysis and preparation. Simulation modeling is performed within the object oriented modeling environment Dymola. This allows the modeling of the satellite dynymics on its most transparent level in form of physical objects, and the modeling of the control algorithm in form of basic control block objects. From the object model of the controlled Equators- S a simulation code is automatically generated for simulating a spin axis erection maneuver using the Shigehara algorithm. Such a maneuver is necessary to ensure constant power supply by solar cells for the rotating satellite independently from the position of sun.

Item URL in elib:https://elib.dlr.de/24188/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1996,
Title:Attitude Control Simulation for Equator-S using Object Oriented Modeling
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Enderle, W.Hauptabteilung RaumflugmissionenUNSPECIFIED
Feucht, U.Hauptabteilung RaumflugmissionenUNSPECIFIED
Moormann, D.Institut für Dynamik der FlugsystemeUNSPECIFIED
Date:1996
Journal or Publication Title:Proceedings 3rd ESA International Conference on Spacecraft Guidance, Navigation and Control Systems
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmail
ESA, UNSPECIFIED
Status:Published
Keywords:Attitude Control, Object Oriented Modeling, Simulation, Equator-S, Dymola
Event Title:3rd ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, ESA-ESTEC, Noordwijk, 26.28.11.1996
Organizer:ESA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W SY - Technik für Raumfahrtsysteme
DLR - Research area:Space
DLR - Program:W SY - Technik für Raumfahrtsysteme
DLR - Research theme (Project):UNSPECIFIED
Location: Oberpfaffenhofen
Institutes and Institutions:Space Operations and Astronaut Training > Hauptabteilung Raumflugmissionen
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 05:21

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