| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1715487 | Acta Astronautica | 2012 | 10 Pages |
Abstract
⺠Different attitude control modes are proposed to perform an inspection mission. ⺠The relative orbit is described by the Hill-Clohessy-Wiltshire equation. ⺠Inspection within a FOV is demonstrated under inertial or nadir pointing. ⺠A target tracking controller of the relative attitude is proposed. ⺠Relative attitude control is feasible within realistic torque limitations.
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Authors
Nadjim M. Horri, Kristian U. Kristiansen, Phil Palmer, Mark Roberts,