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作 者:谷雨 司帆 赵剡[2] 张亚崇[1,3] GU Yu;SI Fan;ZHAO Yan;ZHANG Yachong(Xi'an Flight Automatic Control Research Institute,Xi'an 710065,China;School of Instrumentation Science and Opto-electronic Engineering,Beihang University,Beijing 100191,China;National Key Laboratory on Flight Vehicle Control Integrated Technology,Xi'an 710065,China)
机构地区:[1]西安飞行自动控制研究所,西安710065 [2]北京航空航天大学仪器科学与光电工程学院,北京100191 [3]飞行器控制一体化技术国防科技重点实验室,西安710065
出 处:《弹箭与制导学报》2018年第1期41-44,48,共5页Journal of Projectiles,Rockets,Missiles and Guidance
基 金:装备预研基金资助
摘 要:针对机载武器传递对准中杆臂效应动态补偿这一技术难题,提出了一种改进的杆臂效应动态补偿方法。通过建立机翼的挠曲模型,得到挠曲变形作用下的标称动态杆臂矢量;结合动态杆臂,详细分析了杆臂效应的动态补偿机理;采用"速度+姿态"匹配传递对准模型对所提方法进行了分析与验证。仿真结果表明,所提方法能够有效解决杆臂效应的动态补偿问题。In order to solve the technical problem that the dynamic compensation for lever arm effect in transfer alignment of airborne weapon,an improved dynamic compensation method for lever arm effect was proposed.Firstly,through the establishment of the flexure model of wing,the nominal dynamic lever arm vector under flexural deformation was obtained.Then,combining with the dynamic lever arm,the dynamic compensation mechanism of lever arm effect was analyzed in detail.Finally,the proposed method was analyzed and validated by using the "velocity plus attitude" matching transfer alignment model.The simulation results show that the proposed method can effectively solve the dynamic compensation problem of lever arm effect.
关 键 词:机载武器 传递对准 挠曲变形 杆臂效应 速度+姿态匹配
分 类 号:V271.4[航空宇航科学与技术—飞行器设计] V249.32
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