| 无人攻击机垂直命中目标末制导律研究 |
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| 引用本文： | 刘子阳,黄长强,翁兴伟.无人攻击机垂直命中目标末制导律研究[J].飞行力学,2008,26(6). |
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| 作者姓名： | 刘子阳 黄长强 翁兴伟 |
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| 作者单位： | 1. 空军工程大学,工程学院,陕西,西安,710038;中国人民解放军,94831部队,浙江,衢州,324000
2. 空军工程大学,工程学院,陕西,西安,710038 |
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| 摘 要： | 在充分考虑无人攻击机自动驾驶仪动态因素的基础上,设计了一种能够垂直命中目标的末制导律.该制导律较大程度地改善了无人攻击机终端命中角问题,同时大大提高了无人机的攻击精度,提高了作战效能.仿真结果表明,该导引律满足电视制导无人机的战技指标要求,具有一定的工程实用价值.
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| 关 键 词： | 无人攻击机 制导律 制导与控制 |
Study on the Terminal Guidance System of Hitting the Target Vertically for UCAV |
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| LIU Zi-yang,HUANG Chang-qiang,WENG Xing-wei.Study on the Terminal Guidance System of Hitting the Target Vertically for UCAV[J].Flight Dynamics,2008,26(6). |
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| Authors: | LIU Zi-yang HUANG Chang-qiang WENG Xing-wei |
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| Institution: | 1.Engineering Institute;Air Force Engineering University;Xi'an 710038;China;2.94831 Unit of the PLA;Quzhou 324000;China |
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| Abstract: | Considering the attack process of the television homing UCAV and dynamics factors of an autopilot,a control law of terminal phase,which can hit a target vertically,is designed.The method thinks the impact attitude angle restriction as a question of target following,eliminating the gravity influence,and holds the UCAV hitting the target vertically,which enhances the operational effectiveness.At last by the digital simulation,the feasibility and validity of the terminal guidance are proved. |
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| Keywords: | UCAV guidance law guide and control |
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