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作 者:倪新国[1] 胡正东[1] 张士峰[1] 杨华波[1]
机构地区:[1]国防科学技术大学航天与材料工程学院,湖南长沙410073
出 处:《上海航天》2009年第3期42-46,共5页Aerospace Shanghai
摘 要:根据建立的传递对准模型和用于导航解算的轨道运动学模型,提出了速度匹配、比力匹配、角速率匹配和姿态匹配等空间平台武器系统传递对准的不同匹配方式,并对不同匹配方式及其组合的传递对准性能进行了仿真分析,研究了弹性变形的影响。结果表明:速度+角速率和比力+姿态等组合匹配方式的传递对准性能较优。According to the transfer alignment model established and the orbit kinematics model for navigation calculation, various matching manners of transfer alignment for weapon system on space platform, such as velocity matching, force matching, angular rate matching and attitude matching, were discussed in this paper. The transfer alignment performances of various matching manners and different combinations were analyzed through simulation, in which the impact of the wing flexure on the transfer alignment performances was discussed. The results showed that the integrated matching manners such as velocity + angular rate matching or force +attitude matching had better transfer alignment performance.
关 键 词:空间平台 武器系统 传递对准 轨道机动 弹性变形
分 类 号:U666.1[交通运输工程—船舶及航道工程]
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