Research Article

Satellite Attitude Control Using Analytical Solutions to Approximations of the Hamilton-Jacobi Equation

Table 1

Controller disturbance rejection.

PD Optimal SOS
(1st-order) (2nd-, 3rd-, and 4th-order) (both) (CL)

( ) 10.809686 10.809683 1.989095 5.328614 1.319846
(N·m) ( ) 3.979559 3.979559 3.977874 3.977763 3.976904