Guidance and Robust Gyromoment Precise Attitude Control of Agile Observation Spacecraft-Reference-Cited by-同舟云学术

Guidance and Robust Gyromoment Precise Attitude Control of Agile Observation Spacecraft

Published:2008 Issue:2 Volume:41 Page:3422-3427
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Somov Ye.,Butyrin S.,Somov S.

Publisher

Elsevier BV

Subject

General Medicine

Reference9 articles.

1. Application of Quaternions for Problems of Rigid Body Attitude;Branetz,1973

2. Optimal open-loop and feedback control using single gimbal control moment gyroscopes;Hoelscher;Journal of the Astronautical Sciences,1994

3. Optimal Spacecraft Rotational Maneuvers;Junkins,1986

4. Ye.I. Somov. Analytic synthesis of a programme gyromoment conrol by free-flying space robot. Conrol Problems, (6):72–78, 2006.

5. Optimization of a rotation maneuver and synthesis of gyromoment guidance laws for spacecraft and free-flying robots;Somov;Izvestiya of Samara Scientific Center RAS,2007

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