| 变目标方位角导引法 |
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| 引用本文： | 屠巴宁 宋子善. 变目标方位角导引法[J]. 北京航空航天大学学报, 1997, 23(6): 703-707 |
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| 作者姓名： | 屠巴宁 宋子善 |
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| 作者单位： | 北京航空航天大学自动控制系 |
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| 摘 要： | 研究一种用于近程弹道式地－地弹的导引法，它是借用空－空弹常值目标方位角导引法的概念，把它改变成按弹道设计需要而变化的目标方位角导引法，去攻击地面固定目标，它有减小气动阻力，提高命中相对精度的优点，称它为变目标方位角导引法。
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| 关 键 词： | 导引法 SINS 变目标方位角 组合导引 地地导弹 |
GUIDANCE METHOD OF VARIATIONAL TARGET ORIENTATION ANGLE |
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| Tu Baning Song Zishan. GUIDANCE METHOD OF VARIATIONAL TARGET ORIENTATION ANGLE[J]. Journal of Beijing University of Aeronautics and Astronautics, 1997, 23(6): 703-707 |
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| Authors: | Tu Baning Song Zishan |
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| Abstract: | In order to guide the short range ballistic s s missile with little relative error to traget,we has studied the guidance mothod of variational target orientation angle.It changes from the conception of guidance method with constant target orientation angle for A A missile.And it nas too the advance of small darg for flying missile. |
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| Keywords: | range absolute error relative error standard trajectory variational target orientation angle |
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