Review of Attitude Representations Used for Aircraft Kinematics
- 1 July 2001
- journal article
- review article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 38 (4) , 718-737
- https://doi.org/10.2514/2.2824
Abstract
No abstract availableThis publication has 82 references indexed in Scilit:
- Sliding mode control using modified Rodrigues parametersJournal of Guidance, Control, and Dynamics, 1996
- Global stabilization of flexible multibody spacecraft using quaternion-based nonlinear control lawJournal of Guidance, Control, and Dynamics, 1996
- REQUEST - A recursive QUEST algorithm for sequential attitude determinationJournal of Guidance, Control, and Dynamics, 1996
- Attitude determination and control of Clementine during lunar mappingJournal of Guidance, Control, and Dynamics, 1996
- Derivation of the relative quaternion differential equationJournal of Guidance, Control, and Dynamics, 1991
- The number of multiplications required to chain coordinate transformationsJournal of Guidance, Control, and Dynamics, 1985
- New results on the optimal spacecraft attitude maneuver problemJournal of Guidance, Control, and Dynamics, 1984
- Kalman Filtering for Spacecraft Attitude EstimationJournal of Guidance, Control, and Dynamics, 1982
- Improved Local Linearization Algorithm for Solving the Quaternion EquationsJournal of Guidance and Control, 1980
- Kinematical equations for bodies whose rotation is described by the Euler-Rodrigues parameter.AIAA Journal, 1968