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惯导系统传递对准精度实验的半物理仿真方案
引用本文:鲁浩,徐世杰,徐剑芸. 惯导系统传递对准精度实验的半物理仿真方案[J]. 测试技术学报, 2007, 21(3): 225-231
作者姓名:鲁浩  徐世杰  徐剑芸
作者单位:北京航空航天大学,宇航学院,北京,100083;中国空空导弹研究院,河南,洛阳,471009;北京航空航天大学,宇航学院,北京,100083;中国空空导弹研究院,河南,洛阳,471009
摘    要:提出了一种惯导系统传递对准精度试验的半物理仿真方案,该方案可用于评估空空导弹捷联惯导系统的传递对准精度.该半物理仿真系统模拟空中传递对准的"真实过程",评估出导弹惯导系统相对于基准系统的失准角,搭建了给予该方案的半物理仿真试验系统.经在某型惯导产品的传递对准精度试验中的实际应用,表明该方案是可行的和实用的.

关 键 词:空空导弹  捷联惯导  传递对准  平物理仿真
文章编号:1671-7449(2007)03-0225-07
收稿时间:2006-11-19
修稿时间:2006-11-19

Research on Semi-Physical Simulation Technology for the Transfer Alignment Test of Inertial Navigation Systems
LU Hao,XU Shi-jie,XU Jian-yun. Research on Semi-Physical Simulation Technology for the Transfer Alignment Test of Inertial Navigation Systems[J]. Journal of Test and Measurement Techol, 2007, 21(3): 225-231
Authors:LU Hao  XU Shi-jie  XU Jian-yun
Abstract:This paper proposed a semi-physical simulation plan for evaluating the transfer alignment accuracy test of the strapdown inertial navigation system of an air-to-air missile. It simulates the actual process of transfer alignment in air and evaluates the error angle between a missile inertial navigation system and a reference system. Based on the semi-physical simulation plan, a testing system was constructed. The plan has been used in a practical missile inertial navigation system, which validated the feasibility and practicability of the plan.
Keywords:air to air missile   strapdown inertial navigation   transfer alignment   semi-physical simulation
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