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国外组合式INS/GPS系统研制开发情况两三例 被引量:1

Some Examples of Integrated INS/GPS System Development at Abroad
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摘要 组合式INS/GPS系统可以满足各种导航要求的应用,包括飞机、靶机和导弹。本报告介绍了几个实例来反映国外研制、试验和开发组合式INS/GPS系统的近况。 Integrated INS/ GPS System can satisfy applications of a variety of navigation requirements, including aircraft, target drone and missile. In this paper some examples are introduced to illustrate recent research, test and development of integrated INS/ GPS System at abroad.
作者 汪锡帧
出处 《航天控制》 CSCD 北大核心 1994年第3期53-59,共7页 Aerospace Control
关键词 惯性导航系统 卡尔曼滤波器 飞机 导弹 GPS Global positioning system Inertial navigation system Kalmanfilter Aircraft Missile.
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  • 1卞鸿巍,金志华.联合直接攻击弹药精确制导技术分析[J].中国惯性技术学报,2004,12(3):76-80. 被引量:6
  • 2孙荣忠.美军新一代精确制导导弹[J].国防科技,2005,26(3):9-12. 被引量:4
  • 3Harold A Klitz,Jr Charles B Derbak. The Boeing company GPS-aided navigation and unaided navigation on the Joint Direct Attack Munitions. Position Location and Navigation Symposium, 20-23 April 1998:412 -419.
  • 4Hyslop G Gerth D, Kraemer J. GPS/INS integration on the Standoff Land Attack Missile (SLAM). Aerospace and Electronic Systems Magazine, IEEE Volume 5, Issue 7, July 1990:29 - 34.
  • 5Jongyuk Kim, Salah Sukkarieh. 6DoF SLAM aided GNSS/INS navigation in GNSS denied and unknown environments. Journal of Global Position System, 2005, Vol4 : 120-128.
  • 6Hide C, Moore T, Smith M. Adaptive Kalman filtering algorithms for integrating GPS and low cost INS. Position ocation and Navigation Symposium, 2004. 26-29 April 2004:227 - 233.
  • 7Christopher C Ross, Timothy F Elbert. A transfer alignment algorithm study based on actual flight test data from a tactical air-to-ground weapon launch. Position Location and Navigation Symposium, IEEE 1994. 11-15 April 1994:431 -438.
  • 8陈晓阳,宋晓珏,沈雪瑾,王小静.蟹脚型微谐振器的横向振动分析[J].机械工程学报,2001,37(7):37-40. 被引量:15
  • 9刘危,解旭辉,李圣怡.微机械惯性传感器的技术现状及展望[J].光学精密工程,2003,11(5):425-431. 被引量:35

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