๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Attitude Control of Space Platform Based Tethered Satellite System

โœ Scribed by Modi, Vinod J.; Gilardi, Gabriele; Misra, Arun K.


Book ID
121077585
Publisher
American Society of Civil Engineers
Year
1998
Tongue
English
Weight
730 KB
Volume
11
Category
Article
ISSN
0893-1321

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Nonlinear control of tethered satellite
โœ Monica Pasca ๐Ÿ“‚ Article ๐Ÿ“… 1997 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 702 KB

The control of in-plane transversal vibrations of a tethered satellite system by means of a longitudinal force exerted by subsatellite thrusts is analyzed. A one-mode model is derived for describing the inplane dynamics of such a system. On the basis of this model, two different nonlinear (and simpl

Control of the vibrations of a tethered
โœ F. Dignath; W. Schiehlen ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 613 KB

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

Attitude control system of Molniya 1 com
โœ B.V. Raushenbakh; Je N. Tokar ๐Ÿ“‚ Article ๐Ÿ“… 1971 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 644 KB

Attitude control of the Molniya I communication satellite which moves in a high eceentfic, periodically corrected orbit, and is continuously facing the Sun with its solar panels and the Earth with its antenna, is a difficult problem. It is shown that this problem may be solved by means of the multi-