| dc.contributor.author | Oland, Espen | |
| dc.date.accessioned | 2018-03-13T08:16:27Z | |
| dc.date.available | 2018-03-13T08:16:27Z | |
| dc.date.issued | 2017-08-08 | |
| dc.description.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 | en_US |
| dc.description | Embargoed OA, manuscript version after 24 months from publishing date.
Link to publishers version: <a href=http://doi.org/10.1109/RAST.2017.8002983>http://doi.org/10.1109/RAST.2017.8002983</a> | en_US |
| dc.identifier.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 | en_US |
| dc.identifier.cristinID | FRIDAID 1568360 | |
| dc.identifier.doi | 10.1109/RAST.2017.8002983 | |
| dc.identifier.isbn | 978-1-5386-1605-5 | |
| dc.identifier.uri | https://hdl.handle.net/10037/12298 | |
| dc.language.iso | eng | en_US |
| dc.publisher | Institute of Electrical and Electronics Engineers (IEEE) | en_US |
| dc.rights.accessRights | openAccess | en_US |
| dc.subject | VDP::Technology: 500 | en_US |
| dc.subject | VDP::Technology: 500::Electrotechnical disciplines: 540 | en_US |
| dc.title | Attitude Determination and Control System for Satellites in Elliptical Orbits - a Complete Solution | en_US |
| dc.type | Konferansebidrag | no |
| dc.type | Conference object | en_US |
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