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.
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.
出处
《测试技术学报》
2007年第3期225-231,共7页
Journal of Test and Measurement Technology
关键词
空空导弹
捷联惯导
传递对准
平物理仿真
air to air missile
strapdown inertial navigation
transfer alignment
semi-physical simulation
