| 舰空导弹协同制导交接班形势判断 |
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| 引用本文： | 代进进,李相民,黎子芬.舰空导弹协同制导交接班形势判断[J].飞行力学,2012,30(4):380-384. |
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| 作者姓名： | 代进进 李相民 黎子芬 |
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| 作者单位： | 1. 海军航空工程学院研究生管理大队,山东烟台,264001
2. 海军航空工程学院兵器科学与技术系,山东烟台,264001 |
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| 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。
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| 关 键 词： | 舰空导弹 协同制导 交接班形势 弹道解算 |
Shifting situation judgment of coordinated guidance for ship-to-air missile |
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| DAI Jin-jin
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LI Xiang-min
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LI Zi-fen.Shifting situation judgment of coordinated guidance for ship-to-air missile[J].Flight Dynamics,2012,30(4):380-384. |
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| Authors: | DAI Jin-jin LI Xiang-min LI Zi-fen |
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| Institution: | 1 (1.Graduate Students’ Brigade,NAAU,Yantai 264001,China; 2.Department of Ordnance Science Technology,NAAU,Yantai 264001,China) |
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| Abstract: | 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. |
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| Keywords: | ship-to-air missile cooperative guidance shift situation trajectory calculation |
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