Unified kinematic framework for a non-nominal Euler axis/angle rotation

Author:

de Angelis E.L.,Giulietti F.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference10 articles.

1. Quarternion feedback regulator for spacecraft eigenaxis rotations;Wie;J. Guidance, Control, Dyn.,1989

2. Optimal rotation angle about a non-nominal Euler axis;Giulietti;J. Guidance, Control, Dyn.,2007

3. Constrained slews for single-axis pointing;Avanzini;J. Guidance, Control, Dyn.,2008

4. E.L. de Angelis, F. Giulietti, Kinematic equations of non-nominal Euler axis/angle rotation, IAA-AAS-DyCoSS2-14-10-01, in: Proceedings of the 2nd IAA Conference on Dynamics and Control of Space Systems, Rome, Italy, 24–26 March, 2014.

5. Global magnetic attitude control of inertially pointing spacecraft;Lovera;J. Guidance, Control, Dyn.,2005

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