【摘要】 研究了敏捷导弹六自由度导弹动力学建模和仿真问题。首先给出了用于拦截器的姿控脉冲发动机和用于空空导弹敏捷转弯的反作用喷气控制系统的力学模型 ,然后给出了带干扰 (包括风的干扰 )的具有大迎角大姿态机动能力的敏捷导弹的六自由度动力学模型 ,最后利用上述模型对先进空空导弹的越肩发射进行了仿真 ,并给出了部分结果。该模型除了可以进行一般的导弹动力学仿真外 ,尤其适用于空空导弹敏捷转弯 (含越肩发射 )、高空弹道导弹拦截器的大姿态机动等的仿真计算。更多还原

【Abstract】 The 6 DOF model of an agile missile with high angle of attack and high attitude maneuverability with impulse control or reaction jets control system(RJC) is described in this paper. First the total force and moment of the jets are presented for simulation and control of the missile with zero and some constant rolling rate. Then the equations of the 6 DOF model are represented with disturbance including wind. At last a simulation of an air to air missile for the over the shoulder mission is carried out with the model described above and some results are given. This model can be applied to general missile dynamics simulation; it is especially applicable for the simulation of an agile turn of an advanced air to air missile or the maneuvering of a highly maneuverable ballistic missile interceptor.更多还原