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ATTITUDE DETERMINATION AND CONTROL OF THE ASTEROIDFINDER MISSION

Heidecker, Ansgar and Schlotterer, Markus and Theil, Stephan and Hallmann, Marcus (2009) ATTITUDE DETERMINATION AND CONTROL OF THE ASTEROIDFINDER MISSION. 21st International Symposium on Space Flight Dynamics, 28. Sep. - 02. Oct. 2009, Toulouse.

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Abstract

This paper presents concept and design of the attitude control system for the AsteroidFinder/SSB satellite. It describes the results that were obtained during Phase 0/A and extended Phase A of the project. The general system configuration is described and algorithms for attitude determination and control are presented. The base line design is an error state unscented KALMAN filter for the attitude determination and a linear quadric regulator approach for attitude control algorithm. Both algorithms have been integrated into a simulation environment for closed loop test and first results are presented.

Item URL in elib:https://elib.dlr.de/63447/
Document Type:Conference or Workshop Item (UNSPECIFIED)
Title:ATTITUDE DETERMINATION AND CONTROL OF THE ASTEROIDFINDER MISSION
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Heidecker, AnsgarUNSPECIFIEDhttps://orcid.org/0000-0002-7483-9074
Schlotterer, MarkusUNSPECIFIEDUNSPECIFIED
Theil, StephanUNSPECIFIEDUNSPECIFIED
Hallmann, MarcusUNSPECIFIEDUNSPECIFIED
Date:2 October 2009
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Attitude Control, KALMAN filter, AsteroidFinder
Event Title:21st International Symposium on Space Flight Dynamics
Event Location:Toulouse
Event Type:international Conference
Event Dates:28. Sep. - 02. Oct. 2009
Organizer:CENTRE NATIONAL D'ETUDES SPATIALES
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Proj. AsteroidenFinder - Spacebus (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems
Deposited By: Heidecker, Dipl.-Ing. Ansgar
Deposited On:22 Feb 2012 11:21
Last Modified:06 Apr 2017 12:30

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