Minimum Time Control of Flexible Spacecraft by Hamilton's Principle
โ Scribed by A. Di Meglio; A. Ercoli Finzi
- Book ID
- 111532708
- Publisher
- Springer Netherlands
- Year
- 1997
- Tongue
- English
- Weight
- 184 KB
- Volume
- 32
- Category
- Article
- ISSN
- 0025-6455
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
A three-dimensional rest-to-rest attitude maneuver of ยฏexible spacecraft equipped with onยฑo reaction jets is studied. Equations of motion of the spacecraft are developed by using Lagrangian formulation. The ยฎnite element method is used to discretize elastic deformations of a particular model of sate
In this paper, the equations of motion for a non-linearly constrained flexible manipulator with a tip mass are derived by using Hamilton's principle. Dynamic formulation is based on expressing the kinetic and potential energies of the manipulator system in terms of generalized co-ordinates. Four dyn