| 组合制导弹道导弹无依托快速发射技术研究 |
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| 引用本文： | 鲜勇,肖龙旭,李刚.组合制导弹道导弹无依托快速发射技术研究[J].宇航学报,2010,31(8). |
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| 作者姓名： | 鲜勇 肖龙旭 李刚 |
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| 作者单位： | 1. 第二炮兵工程学院603教研室,西安,710025
2. 第二炮兵装备研究院,北京,100085 |
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| 摘 要： | 具有快速机动发射能力的弹道导弹是现代远程作战武器的重要标志,提出了无依托快速发射的定位、定向方案,设计了基于空中在线诸元计算的摄动制导方法,该方法具有计算量小、制导方法误差小的特点,可满足陆基机动弹道导弹或潜射弹道导弹的快速发射的要求。
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| 关 键 词： | 无依托发射 在线诸元计算 组合制导 摄动制导 |
Research on Offhand Fast Launch Technique for Integrated Guidance Ballistic Missile |
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| XIAN Yong,XIAO Long-xu,LI Gang.Research on Offhand Fast Launch Technique for Integrated Guidance Ballistic Missile[J].Journal of Astronautics,2010,31(8). |
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| Authors: | XIAN Yong XIAO Long-xu LI Gang |
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| Institution: | XIAN Yong1,XIAO Long-xu2,LI Gang1(1.Faculty 603,The Second Artillery Engineering College,Xi'an 710025,China,2.The Equipment Research Institute of PLA's Second Artillery,Beijing 100085,China) |
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| Abstract: | The ballistic missile with fast mobile launch capability is the important symbol of modern long-range weapon.In this paper,the positioning and orientation scheme of offhand fast launch is submitted,and the perturbation guidance method based on air online data computation is designed.The small computation load and guidance method error of the proposed method can meet the fast launch requirements for ground-based mobile ballistic missile and submarine-launched ballistic missile. |
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| Keywords: | Offhand launch Online data computation Integrated guidance Perturbation guidance |
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