Attitude Dynamics of Satellites with Flexible Appendages- A Brief Review
- 1 November 1974
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 11 (11) , 743-751
- https://doi.org/10.2514/3.62172
Abstract
No abstract availableThis publication has 87 references indexed in Scilit:
- Liapunov Stability Analysis of Hybrid Dynamical Systems in the Neighborhood of Nontrivial EquilibriumAIAA Journal, 1974
- A form of the translational dynamical equations for relative motion in systems of many non-rigid bodiesActa Mechanica, 1972
- Liapunov stability of spinning satellites with long flexible appendagesCelestial Mechanics and Dynamical Astronomy, 1971
- Variational Equation of Motion for Coupled Flexure and Torsion of Bars of Thin-Walled Open Section Including Thermal EffectJournal of Applied Mechanics, 1971
- Dynamical equations of nonrigid satellitesAIAA Journal, 1970
- Basic relations for control of flexible vehiclesAIAA Journal, 1970
- Use of synthetic modes in hybrid coordinate dynamic analysis.AIAA Journal, 1968
- Exploitation of nonlinear resonance in damping an elastic Dumbbell satellite.AIAA Journal, 1968
- Some remarks on the dynamics of deformable bodies.AIAA Journal, 1968
- An analytical representation of temperature distributions in gravitygradient rods.AIAA Journal, 1968