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直升机综合外挂梁动态扰动响应对武器精度影响分析

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直升机综合外挂梁的动态响应会引起武器初始发射状态的六自由度偏差进而影响武器打击精度。提出一种误差环面积偏差的误差分析方法;结合地理坐标系和载机武器坐标系间的转换关系,推导出误差环的解析方程,并给出误差环面积偏差的详细解算方法;结合算例分析出误差环的变化特点及偏差精度。
Analysis of the Influence of Dynamic Disturbance Response of Integrated External Hanging Beam of a Helicopter on Weapon Accuracy
The dynamic response of the integrated external hanging beam of a helicopter will cause the 6-degree-of-freedom deviation of the initial launching state of the weapon,which will affect the striking accuracy of the weapon.An error analysis method of error donut area deviation is proposed.Combined with the conversion relationship between the geographic coordinate system and the aircraft weapon coordinate system,the analytical equation of the error donut is derived,and the detailed solution method of the error donut area deviation is given.Finally,the variation characteristics and deviation accuracy of the error donut are analyzed with examples.

helicoptersintegrated external hanging beamweapon accuracycoordinate transformationdynamic response

严鹏辉、刘刚、郭晓利

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中国直升机设计研究所,天津 300300

中国飞行试验研究院,西安 710089

直升机 综合外挂梁 武器精度 坐标变换 动态响应

2024

火力与指挥控制
火力与指挥控制研究会,火力与指挥控制专业情报网

火力与指挥控制

CSTPCD北大核心
影响因子:0.312
ISSN:1002-0640
年,卷(期):2024.49(11)