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ANALYSIS OF LEVER ARM EFFECTS IN GPS/IMU INTEGRATION SYSTEM 被引量:8
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作者 liujianye HeXiufeng 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2002年第1期59-64,共6页
Disturbance specific force caused by the lever arm ef-fects in integration navigation system is investigated,Navigation errors eaused by the lever arm effects have been demonstrated under three flinght scenarios of th... Disturbance specific force caused by the lever arm ef-fects in integration navigation system is investigated,Navigation errors eaused by the lever arm effects have been demonstrated under three flinght scenarios of the air-craft.Analytical under three flight scenarios of the ari-craft.Analytical results show that disturbance specific force resulted from lever arm effects may become one of the major error sources while an aircraft undertakes the maneuvers,and mavigation errors caused by the lever arm effects accumulate rapidly with time.Therefore,a com-pensation method must be taken into account to eliminate the disturbance specific force caused by the lever arm ef-fects in integration navigation system. 展开更多
关键词 GPS INS lever arm error ANALYSIS simula-tion 全球定位系统 惯性导航系统 飞机 杆臂效应 导航误差 组合导航系统
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