Problems on health checking a control system for the spacecraft orientation in initial modes are considered – during their separation from a launcher rocket up to regular attitude stabilization in orbital reference frame. Developed methods, algorithms and the simulation results on the initial orientation modes of the small satellites and space robots are presented.
Health Checking of a Spacecraft Control System in the Orientation Initial Modes
01.06.2019
1355744 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Spacecraft attitude guidance and economical digital control in initial modes
American Institute of Physics | 2018
|Spacecraft attitude pulse-width control at initial, service and emergency modes
American Institute of Physics | 2012
|Spacecraft attitude pulse-width control at initial, service and emergency modes
British Library Conference Proceedings | 2012
|