ABSTRACT
A simple state feedback method for satellite trajectory design on a halo orbit is developed. The communication link using satellite trajectory control is from the earth to the satellite and then to the far side of the moon. The nonlinearities inherent to the halo orbit problem are treated as trajectory-dependent, persistent disturbance inputs.
A controller has been designed along with a full order estimator of linear state variable feedback using pole placement method. This type of compensated linear controllers gives satisfactory performance for limited dynamic range and limited input. The design has been made by specially constructed programs and the results have been checked up using MATLAB tools.
