Title: | Attitude estimation of a small spinning satellite using Kalman filter approaches |
Author(s): | Khurshid, Osama |
Date: | 2017 |
Language: | en |
Pages: | 113 |
Department: | Elektroniikan ja nanotekniikan laitos Department of Electronics and Nanoengineering |
ISBN: | 978-952-60-7503-7 (electronic) 978-952-60-7504-4 (printed) |
Series: | Aalto University publication series DOCTORAL DISSERTATIONS, 122/2017 |
ISSN: | 1799-4942 (electronic) 1799-4934 (printed) 1799-4934 (ISSN-L) |
Supervising professor(s): | Kallio, Esa, Asst. Prof., Aalto University, Department of Electronics and Nanoengineering, Finland |
Thesis advisor(s): | Selkäinaho, Jorma, Dr., Aalto University, Department of Electrical Engineering and Automation , Finland |
Subject: | Electrical engineering |
Keywords: | satellite, spacecraft, attitude dynamics, attitude estimation, system design, Kalman filter, UKF, PSLKF |
Archive | yes |
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Abstract:Nanosatellites provide a low-cost solution to designing, developing and building space systems. However, there are several constraints linked to the low-cost, compact size and quick development time of such nanosatellites. These cost constraints restrict the use of space-grade reliable hardware. These factors lead to the risks pertaining to the reliability and robustness of the system. The Attitude Determination and Control System (ADCS) is one of the subsystems for which both the hardware and the software are affected by the adverse effects of the closely integrated subsystems.
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