Flight Results of ESTCube-1 Attitude Determination System
This paper presents the characterization and in-orbit validation of the ESTCube-1 attitude determination system (ADS). ESTCube-1 is a one-unit CubeSat built by students and launched on May 7, 2013, to a Sun-synchronous, 700-km, polar low Earth orbit. Its primary mission is to centrifugally deploy a tether as a part of the first in-orbit demonstration of electric solar wind sail (i.e., E-sail) technology. The ADS uses magnetometers, gyroscopic sensors, Sun sensors, and an unscented Kalman filter for attitude determination. Here the performance of commercial off-the-shelf (COTS) sensors and results from tuning the system is shared; recalibration, software, and Kalman filter adjustments. The system is validated by comparing the attitude determined by the on-board ADS with the attitude determined from on-board camera images. Uncertainty budgets for both attitude determination methods are estimated. The expanded uncertainty of comparison (95% confidence level, k=2) is 1.75° and the maximum difference between attitudes determined by both methods is 1.43°.
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Availability:
- Find a library where document is available. Order URL: http://worldcat.org/issn/08931321
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Supplemental Notes:
- © 2015 American Society of Civil Engineers.
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Authors:
- Slavinskis, Andris
- Ehrpais, Hendrik
- Kuuste, Henri
- Sünter, Indrek
- Viru, Jaan
- Kütt, Johan
- Kulu, Erik
- Noorma, Mart
- Publication Date: 2016-1
Language
- English
Media Info
- Media Type: Web
- Features: References;
- Pagination: 04015014
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Serial:
- Journal of Aerospace Engineering
- Volume: 29
- Issue Number: 1
- Publisher: American Society of Civil Engineers
- ISSN: 0893-1321
- EISSN: 1943-5525
- Serial URL: http://ascelibrary.org/journal/jaeeez
Subject/Index Terms
- TRT Terms: Artificial satellites; Flight attitude; Kalman filtering; Sensors
- Uncontrolled Terms: Solar wind
- Subject Areas: Aviation; Vehicles and Equipment; I90: Vehicles;
Filing Info
- Accession Number: 01561482
- Record Type: Publication
- Files: TRIS, ASCE
- Created Date: Apr 27 2015 9:49AM