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GPS/IMU组合导航系统中杆臂效应分析(英文)
引用本文:何秀凤,刘建业.GPS/IMU组合导航系统中杆臂效应分析(英文)[J].南京航空航天大学学报(英文版),2002(1).
作者姓名:何秀凤  刘建业
作者单位:河海大学科学院,南京航空航天大学自动化学院 南京210098,中国,南京210016,中国
摘    要:研究了组合导航系统中杆臂效应引起的干扰比力问题。文中给出了几种飞行状态下由杆臂效应引起的导航误差。分析表明 ,当飞机作机动飞行时 ,杆臂效应引起的干扰比力是主要的误差源之一 ,并且由干扰比力产生的导航误差随时间快速积累。因此 ,在组合导航系统中必需考虑在线的补偿方法 ,以便补偿由杆臂效应引起的导航误差。

关 键 词:全球定位系统  惯性导航系统  杆臂效应  误差分析  仿真

ANALYSIS OF LEVER ARM EFFECTS IN GPS/IMU INTEGRATION SYSTEM
He XiufengAcademy of Sciences,Hehai University,Nanjing ,P.R.ChinaLiu Jianye College of Automation Engineering,NUAA Yudao Street,Nanjing ,P.R.China.ANALYSIS OF LEVER ARM EFFECTS IN GPS/IMU INTEGRATION SYSTEM[J].Transactions of Nanjing University of Aeronautics & Astronautics,2002(1).
Authors:He XiufengAcademy of Sciences  Hehai University  Nanjing  PRChinaLiu Jianye College of Automation Engineering  NUAA Yudao Street  Nanjing  PRChina
Institution:He XiufengAcademy of Sciences,Hehai University,Nanjing 210098,P.R.ChinaLiu Jianye College of Automation Engineering,NUAA29 Yudao Street,Nanjing 210016,P.R.China
Abstract:Disturbance specific force caused by the lever arm effects in integration navigation system is investigated. Navigation errors caused by the lever arm effects have been demonstrated under three flight scenarios of the aircraft. 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 navigation errors caused by the lever arm effects accumulate rapidly with time. Therefore, a compensation method must be taken into account to eliminate the disturbance specific force caused by the lever arm effects in integration navigation system.
Keywords:GPS  INS  lever arm  error analysis  simulation
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