期刊文献+

一种四元数更新算法的推导及仿真研究 被引量:9

Proof and Simulation for a Updating Algorithm of Quaternion
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摘要 在捷联惯导系统中,可以用四元数来表示姿态矩阵,而姿态矩阵的计算是捷联惯导系统的关键问题之一。本文引入四元数三阶泰勒展开递推式作为四元数的更新算法,着重进行了公式的推导,并对某陆地捷联惯导系统的实际测量数据进行了仿真,仿真结果表明了该算法的有效性。 Attitude matrix is represented by quaternion and the calculation of attitude matrix is a key in Strapdown INS. In this paper three-order recursive Taylor expanded form of quaternion as the updating algorithm of quaternion is introduced. With the emphasis on the proof of the formula, the paper makes the corresponding simulation to the datum of a land vehicle strapdown INS that has been collected. The result proved that the algorithm is effective.
出处 《系统仿真学报》 CAS CSCD 2002年第4期430-431,446,共3页 Journal of System Simulation
关键词 四元数更新算法 仿真 捷联惯导系统 方向余弦矩阵 quaternion strapdown INS simulation attitude
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参考文献3

  • 1陈哲.全姿态飞机捷联式系统姿态角的计算[J].航空学报,1983,4(3).
  • 2张亚崇,郭圣权.一种捷联惯导系统姿态测量新算法的应用研究[J].火力与指挥控制,2000,25(1):77-80. 被引量:6
  • 3Guo Shengquan, et al. Comparative Research of Several Kinds of the Inertial Attitude Measurement System [A]. International Conference on Intelligent Autonomous Control in Aerospace.1995.

二级参考文献4

  • 1肖尚彬.四元数方法及其应用[J].力学进展,1993,23(2):249-260. 被引量:43
  • 2陈哲.全姿态飞机捷联式系统姿态角的计算[J].航空学报,1983,4(3).
  • 3Sheng Quan,Guo Sheng Quan et al,Comparative Re-search of Several Kinds of theInertial Attitude Measurement System.International Conference on Intelligent AutonomousControl in Aerospace.1995
  • 4U.K.Kromann.Strapdown Attitude and Heading Re-ference for a Class of Medium AlcurayNavigation Systems.Symp.Gyro-Technology,Stuttgart/Germany,Sept.1979

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