A dynamic model of the Tethered Satellite System (TSS) and of the relevant simulation program, developed in order to provide the dynamic analysis support for the design verification of the subsatellite attitude control, is presented. Special care was spent in the satellite attitude dynamic analysis and the model was specifically conceived to this aim. The way in which the simulation results can be utilized for the verification and testing of the attitude control is also presented.
TSS (Tethered Satellite System) Subsatellite Attitude Dynamics and Control Laws Verification Programs
1987
31 pages
Report
No indication
English
NTRS | 1976
|NTIS | 1976
|Optimal control of the Shuttle-Tethered-Subsatellite system
Elsevier | 1980
|