“…The controller objective is then to restore both attitude and angular rates to a zero reference state. The initial conditions on the physical state representing this disturbance are defined as where states (1, 2, 3) are roll, pitch, and yaw in the LVLH reference frame, states (4, 5, 6) are elements of the angular velocity vector, and states (7,8,9) represent angular momentum of each of three reaction microwheels used in control. Because we are regulating states to zero, the reference trajectory is x p,r = 0 0 0 0 0 0 0 0 0 .…”