A new method for the orbital modification of a tether connected satellite system
โ Scribed by A. Djebli; M. Pascal
- Publisher
- Springer Vienna
- Year
- 2004
- Tongue
- English
- Weight
- 349 KB
- Volume
- 167
- Category
- Article
- ISSN
- 0001-5970
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
An orbital tether system, including a satellite (a rigid body), an elastic ponderable tether and a terminal load, is investigated. A mathematical model is obtained using Lagrange's equation of the second kind, which enables the plane translational motion of the centres of mass of the elements of the
A family of implicit methods based on intrastep Chebyshev interpolation has been d 2 developed to integrate initial value problems of the second-order harmonic oscillator form ~ +wy = f(y(t); t). The procedure integrates the homogeneous part exactly (in the absence of roundoff errors). The Chebyshev
A method of damping structural vibrations using optimization techniques is presented and applied to a tethered satellite system. Such systems show large displacements and require active or passive damping mechanisms. A tethered satellite system is modelled by the method of multibody systems using sy
The motion about a centre of mass of a rigid body with a tethered system, designed to launch a re-entry capsule from a circular orbit is considered. In the deployment of the tethered system the direction and value of the tensile strength of the tether vary and, if the point of application of the ten