The comparative analysis of features of gyro-force control of large-scale spacecrafts for three algorithm types

Some results of computer modeling of a flexible spacecraft dynamics with low-frequency elastic oscillations of construction are presented. Three types of algorithms for gyro-force control of the spacecraft are considered: proportional, proportional-differential, and proportional-integrated. Areas of preferable use of these control algorithms (by criterion of control time minimum) are determined at change of the lowest frequency of construction elastic oscillations.