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IMU/磁罗盘/GPS组合导航系统设计 被引量:2

Design of IMU/Compass/GPS Integrated Navigation System
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摘要 设计了一个IMU/GPS/磁罗盘组合导航系统和相应导航算法,针对该系统的特点设计了特殊的静基座对准算法。根据系统元器件的特殊性和以往工作经验,采用渐消记忆Kalman滤波算法对IMU和GPS信息进行组合。跑车实验表明,该系统具有精度高,工作稳定等优点,达到了设计要求。 An IMU/GPS/compass integrated navigation system and its navigation algorithm are designed. Aiming at the characteristics of this system, initial alignment algorithm is designed. According to the parts of apparatus particularity, adaptive Kalman algorithm is adopted for integrating information of IMU and GPS. The experiment results demonstrate that this system meets the expected design demand, and has the expected accuracy and high reliability.
作者 刘准 宋征宇
出处 《航天控制》 CSCD 北大核心 2005年第3期40-42,共3页 Aerospace Control
关键词 惯性测量装置 全球定位系统 组合导航 Inertial measurement unit Global positioning system Combined navigation
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同被引文献12

  • 1高化猛,赵新国,李智.飞行器INS与GPS组合导航系统卡尔曼滤波[J].装备指挥技术学院学报,2007,18(1):59-62. 被引量:6
  • 2杨功流,李士心,姜朝宇.地磁辅助惯性导航系统的数据融合算法[J].中国惯性技术学报,2007,15(1):47-50. 被引量:59
  • 3邓正隆.惯性技[M].哈尔滨:哈尔滨工业大学出版社,2006.
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  • 5Luo P, Pei H L. An autonomous helicopter with vision based navigation [ C ]. International conference on control and automation, IEEE ,2007.
  • 6秦永元.卡尔曼滤波与组合导航原理[M].西安:西北工业大学出版社,2004.
  • 7Robert Wolf, Bemd Eissfeller. A Kalman Filter for The Integration of a Low Cost INS and an Attitude GPS. Institute of Geodesy and Nacigation University FAF Munich
  • 8Christopher Hide, Terry Moore.GPS and Low Cost INS Integration using Commercial Off-theshelf Components. Institute of Engineering, Surveying andSpace Geodensy, University of Nottingham
  • 9Jonathan M. Roberts. Low-cost Flight Control System for a Small Autonomous Helicopter. Proc.2002 Australastian Conference on Robotics and Automation Auckland, 2002,9
  • 10Jong-Hyuk Kim, Stuart Wishart,Salah Sukkarieh. Real-time Navigation, Guidance, and Control of a UAV Using Lowcost Sensors.Australian Centre for Field Robotics University of Sydney, NSW 2006, Australia

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