New approach to attitude/momentum control for the Space Station

Controlling a large flexible structure to mimic a rigid one

“…Then, we can build the control law based on game theories such that the v-reachable set will be zero. There are a number of promising research directions [59][60][61][62][63] that can be taken using the proposed control approach. In order to mitigate the effect of rapid maneuvering of a flexible structure, it is proposed that extra actuators be employed.…”

Comparative study of various control methods for attitude control of a LEO satellite

“…They used a full state feedback LQR ( 2 H ) controller with gain scheduled adaptation. In the paper by Wie and et al, a new approach to control the attitude of the space station has been proposed [7]. This paper develops the general nonlinear model of a low earth orbiting satellite with four thrusters, three magnetic torquers, and a four reaction wheel cluster as actuators, in the next section.…”

Integrated Power and Attitude Control with Spacecraft Flywheels and Control Moment Gyroscopes

“…(7) can I)e shown t() xiv(' rise t() tit(' six relationships etnl)h)y(,d as a t),tsis fi)r control law design ill Hcf. [3].…”