A solution of the time-optimal Euler rotation problem
- 14 August 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Quaternion feedback for spacecraft large angle maneuversJournal of Guidance, Control, and Dynamics, 1985
- Exact nonlinear control of large angle rotational maneuversIEEE Transactions on Automatic Control, 1984
- A New Single-Rotation-Axis Autopilot for Rapid Spacecraft Attitude ManeuversJournal of Guidance and Control, 1979
- Quaternion from Rotation MatrixJournal of Guidance and Control, 1978