Dynamics of gyro-force stabilization of large-scale spacecrafts with use of adjusted PD-algorithm of control
Some problems of computer synthesis of adjusted proportional-differential algorithm parameters for gyro-force control of elastic large-scale spacecraft are considered. It is shown that such algorithm ensures optimum on time control of orientation at infralow frequencies of construction elastic oscillations. The technique of definition of area of such values of partial frequencies in which it is possible to use the simplified algorithm with constant coefficients without a drop of control quality is proposed.