Attitude Determination and Control System for Satellites in Elliptical Orbits - a Complete Solution

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https://hdl.handle.net/10037/12298
DOI
https://doi.org/10.1109/RAST.2017.8002983
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Date
2017-08-08
Type
Konferansebidrag
Conference object

Author
Oland, Espen
Abstract
This paper presents a complete solution to the problem of attitude determination and control for satellites in elliptical orbits. Specifically, it shows how to create the orbital mechanics, account for perturbing gravity torques, create a nonlinear PD+ attitude controller, map the control signal to desired thrust firings, implement magnetic field and Sun vector models, and how to implement a Madgwick filter for attitude determination based on vector measurements
Description
Embargoed OA, manuscript version after 24 months from publishing date. Link to publishers version: http://doi.org/10.1109/RAST.2017.8002983
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Citation
Oland E: Attitude Determination and Control System for Satellites in Elliptical Orbits - a Complete Solution. In: Turkish Force Academy. 2017 8th International Conference on Recent Advances in Space Technologies (RAST) 19-22 June 2017, 2017. IEEE conference proceedings p. 79-84
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