Strapdown Attitude Algorithm Suitable for Rate Gyro
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Strapdown Attitude Algorithm Suitable for Rate Gyro
一种适用于速率陀螺的捷联航姿算法
Issue 5, (2005)
作者机构:
1. ,山西,太原,030051
2. 中北大学机械电子工程系
作者简介:
基金信息:
DOI:
CLC:
Published:2005
稿件说明:
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戚九民, 陈国光, 田晓丽, et al. Strapdown Attitude Algorithm Suitable for Rate Gyro[J]. 2005, (5).
DOI:
戚九民, 陈国光, 田晓丽, et al. Strapdown Attitude Algorithm Suitable for Rate Gyro[J]. 2005, (5).DOI:
Strapdown Attitude Algorithm Suitable for Rate Gyro
摘要
为了能将新型固态速率陀螺应用在常规弹箭上
必须研究超高精度的捷联航姿算法
以适应此特殊的应用环境.应用速率陀螺在当前迭代周期和前次迭代周期内输出的信息提出一种修正算法
推导了该方法在典型圆锥运动下的算法误差.结果表明:在速率输入情况下
与传统算法比较
新算法具有较高的精度和适中的计算复杂度.
Abstract
The new type solid state gyro exports angular rate signals directly.Classical rotation vector attitude algorithms have to integrate angular rate frequently.In this paper
by utilizing the angular rate singals export by rate gyro from the latest and current update periods
a new strapdown attitude algorithm expression is developed and the error of the algorithm under the coning motion is derived too.Simulation results show that
compared to the conventional algorithms
the accuracy of the new algorithm is better and calcuation complexity is moderate.
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references
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