The control process for the fast maneuvers of the responsive spacecraft was taken as the research object, and the rapid decoupling of the attitude control problem was investigated. A comprehensive control strategy which integrates time optimal control and tilt switch curve control was proposed based on the decision tree theory. Furthermore, the control time was taken as the cost function, the three-channel time optimal control strategy was obtained. Compared with other methods, the control time of the proposed strategy is reduced by nearly 10 seconds, and the control precision meets the design requirements. Additionally, control results were compared in case of different control cycles for the controller, and the instructional conclusions were provided for selecting and designing of the control cycle.