Direct Path Method for Flexible Multibody Spacecraft Dynamics
- 1 February 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 14 (2) , 102-110
- https://doi.org/10.2514/3.57167
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Equations of motion for interconnected rigid and elastic bodies: A derivation independent of angular momentumCelestial Mechanics and Dynamical Astronomy, 1975
- Dynamic analysis of a system of hinge-connected rigid bodies with nonrigid appendagesInternational Journal of Solids and Structures, 1973
- Stabilizing a Spinning SkylabIFAC Proceedings Volumes, 1972
- Finite element appendage equations for hybrid coordinate dynamic analysisInternational Journal of Solids and Structures, 1972
- The influence of structural flexibility on the dynamic response of spinning spacecraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- A set of r dynamical attitude equations for an arbitrary n-body satellite having r rotational degrees of freedomAIAA Journal, 1970
- Stability of a spinning body containing elastic parts via Liapunov'sdirect methodAIAA Journal, 1970
- On the Derivation of Equations of MotionJournal of the Society for Industrial and Applied Mathematics, 1965
- Dynamics Analysis of a Two-Body Gravitationally Oriented SatelliteBell System Technical Journal, 1963