导弹末端机动的一体化控制模型

采用过载控制技术，建立了反舰导弹末端机动的一体化控制模型。该模型包括两组控制信号：过载控制信号和质心控制信号。利用该模型控制导弹完成了末端跃升、蛇行、摆式和螺旋等各种机动方式。另外，使控制参数按照一定的规律变化，还实现了摆式和螺旋机动的变异形式。由于导弹的机动能力受到可用过载等指标的限制，因此控制参数必须在合理的范围内取值才能保证末端机动的顺利完成。最后，举例对上述模型进行研究，仿真结果表明了该模型的有效性。

Integrative control model of missiles' terminal maneuver

An integrative control model of terminal maneuvers was constructed for anti-ship missiles,adopting the overload-control technique.The model included two groups of control signals:overload-control signal and mass center control signal.Under the control of the model a missile completed all kinds of terminal maneuvers,for instance,leap,serpentine motion,cycloid maneuver and spiral maneuver.In addition,the variation forms of cycloid maneuver and spiral maneuver were realized by varying the control parameters according to some laws.Because missiles maneuverability was limited by some indexes such as useable overload,the control parameters had to be in a reasonable range so that the terminal maneuvers could be favoringly accomplished.Finally,the simulation examples were illustrated to do research on above control model.The simulation results show the effectiveness of the proposed control model.