期刊文献+

基于多传感器技术的微型飞行器智能组合导航技术研究 被引量:2

Research on Multi-sensor Technique-based Intelligent Integrated Navigation for MAV
下载PDF
导出
摘要 微型飞行器(MAV)尺寸微小,有效载荷低,其机载导航系统在结构与原理上都与传统飞机导航系统有很大的差异,增加了系统设计的难度。提出了一种基于组合传感器技术的MAV分层次导航系统方案。在MAV姿态信息提取中,引入了一种四元数结构下的捷联惯导与GPS组合信息卡尔曼滤波方案。在此基础上,通过研究MAV现有传感器技术下的各类导航方式的适用性、精度以及可靠性,根据MAV导航系统的要求,提出了一种基于多传感器智能组合技术的MAV导航位置信息提取方案。仿真与飞行试验证明,本文的这种基于组合传感器技术的MAV分层次导航具有计算简单,精度高,可靠性好的优点。 Flight control and navigation system design plays an important role in MAV design.Compared with traditional airplane,MAV is quite different and has more technical difficulties in navigation system design because of its small size and low payload.Within the limits of MAV space and payload,we presented a multi-sensor technique based two-stage navigation system.An INS/GPS based Kalman Filter solution was introduced in attitude estimate stage.We studied the precision,applicability and reliability of three kinds...
出处 《宇航学报》 EI CAS CSCD 北大核心 2007年第5期1185-1189,共5页 Journal of Astronautics
基金 江苏省研究生创新计划xm04-53资助项目
关键词 微型飞行器 捷联惯导 组合导航 姿态与位置估计 Micro air vehicle SINS Integrated navigation system Attitude and position estimation
  • 相关文献

参考文献5

  • 1[1]Waszak M R,Davidson J B.Simulation and flight control of an aeroelastic fixed wing micro aerial vehicle[J].AIAA,2002-4875
  • 2[2]Scott M,Ettinger,Michael C,Nechyba and Peter D.lfju.Visionguided flight stability and control for micro air vehicles[J].Advanced Robotics,2003,17(7):617-640
  • 3[4]Greg Welch and Gray Bishop.An introduction to the kalman filter[J].UNC-Chapel Hill,TR 95-041,April 5,2004
  • 4[5]Gebre-Egziabher D,Hayward R C and Powell J D.A low-cost GPS/inertial attitude heading reference system (AHRS) for general aviation applications proceedings of the IEEE position location and navigation symposium[C].Palm Springs,CA,April 1998:518-525
  • 5[6]Derek B,Kingston and Rangal W,Beard.Real-time Attitude and Position Estimation for Small Uavs Using Low-Cost Sensors,AIAA 2004-6488

同被引文献23

引证文献2

二级引证文献10

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部