摘要
根据垂直发射舰空导弹的弹道特性和制导特性,将舰空导弹的弹道分为无控段、转弯段和制导段,分别建立各段弹道的解算模型。在此基础上,给出了舰空导弹协同制导作战条件下交班点位置以及到达交班点剩余时间的计算方法。仿真结果验证了所建立的运动学弹道模型以及交接班形势判断方法的正确性与适应性。
Based on the trajectory and guidance characteristics of the vertical-launched ship-to-air missile,trajectory of the ship-to-air missile is divided into non control phase,turning phase and guiding phase,for which the trajectory calculation model is established respectively.Then,the calculating method for shift point position and time to arrive at the shift point under cooperative guidance is given.The results of simulation verify the correctness and applicability of the kinematics trajectory model and the judgment method of shift situation.
出处
《飞行力学》
CSCD
北大核心
2012年第4期380-384,共5页
Flight Dynamics
基金
国防预研基金资助(4010804040102)
关键词
舰空导弹
协同制导
交接班形势
弹道解算
ship-to-air missile
cooperative guidance
shift situation
trajectory calculation