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In this research, a new control law for the trajectory correction maneuver (TCM) is proposed for a spacecraft assumed to be actuated by a low thruster such as an electric propulsion system. During the cruise phase of an interplanetary mission, trajectory errors accumulate continuously owing to unpredictable perturbation forces. In previous research, TCM algorithms were developed under the assumption...
For the interplanetary mission, the spacecraft must require the trajectory correction maneuver (TCM) to reduce the trajectory error due to the influence of unexpected external perturbation forces. There are many kinds of researches focused on these TCM techniques for the impulsive thrust. Among them, the B-plane targeting method is mainly applied to the interplanetary mission as TCM method. However,...
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