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
2019-06-01
1355744 byte
Conference paper
Electronic Resource
English
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