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Observability Analysis for Spacecraft Attitude Determination using a Single Temperature Sensor

Posielek, Tobias and Reger, Johann (2021) Observability Analysis for Spacecraft Attitude Determination using a Single Temperature Sensor. In: European Control Conference 2021, ECC 2021, pp. 1432-1439. European Control Conference 2021, Rotterdam, Netherlands.

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Abstract

We consider the problem of spacecraft attitude determination using temperature data. Common algorithms fuse multiple temperature measurements to reconstruct the attitude. However, a single sensor already contains a lot of information due to the temperature dynamics inherent to the nonlinear structure. In this work a rigorous observability analysis is carried out to determine the configurations in which the combination of a single temperature sensor with angular velocity measurements is sufficient for estimating the entire attitude. We evaluate the observability properties of the different configurations and give recommendations for the best configurations.

Item URL in elib:https://elib.dlr.de/143585/
Document Type:Conference or Workshop Item (Speech)
Title:Observability Analysis for Spacecraft Attitude Determination using a Single Temperature Sensor
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Posielek, Tobiastobias.posielek (at) dlr.deUNSPECIFIED
Reger, Johannjohann.reger (at) tu-ilmenau.deUNSPECIFIED
Date:2021
Journal or Publication Title:European Control Conference 2021, ECC 2021
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1432-1439
Editors:
EditorsEmailEditor's ORCID iD
Posielek, Tobiastobias.posielek@dlr.deUNSPECIFIED
Status:Published
Keywords:Observers for nonlinear systems, Aerospace
Event Title:European Control Conference 2021
Event Location:Rotterdam, Netherlands
Event Type:international Conference
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 - Project GigaStore
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control
Deposited By: Posielek, Tobias
Deposited On:04 Oct 2021 16:43
Last Modified:08 Oct 2021 10:38

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  • Observability Analysis for Spacecraft Attitude Determination using a Single Temperature Sensor. (deposited 04 Oct 2021 16:43) [Currently Displayed]

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