Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Accelerometer error calibration and compensation method based on rotary mechanism

An accelerometer and rotating mechanism technology, applied in the field of inertial device testing and inertial navigation, can solve the problems of large experiment time, expensive inertial devices, and cumbersome testing process, and achieve the effects of low cost, improved estimation accuracy, and low cost.

Inactive Publication Date: 2010-10-06
BEIHANG UNIV
View PDF0 Cites 35 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The advanced test method described in approach (2) often requires advanced test equipment as the basis. Generally, the test equipment for inertial devices is often expensive, and the test process is cumbersome, requiring a lot of experimental time

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Accelerometer error calibration and compensation method based on rotary mechanism
  • Accelerometer error calibration and compensation method based on rotary mechanism
  • Accelerometer error calibration and compensation method based on rotary mechanism

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention relates to an accelerometer error calibration and compensation method based on a rotary mechanism, which comprises the following steps that: an accelerator is arranged on the rotary mechanism according to a certain requirements; the relationship between the dynamic continuous output of the accelerator and the rotating angle of the rotary mechanism is obtained through the rotation of the rotary mechanism; and a least square method is used for estimating and obtaining the bias, the scale factor, the non-linear error coefficient of the scale factor, the cross-coupling error coefficient and the like of the accelerator. The method uses the rotary mechanism to estimate all error coefficients of the accelerator, and is characterized by accuracy, high efficiency, easy operation, high universality and the like. After the method estimates the error coefficients and carries out corresponding error compensation, the output precision of the accelerator can be greatly improved. The method is also applicable to the calibration of a gyroscope, and can greatly improve the precision in measuring the speed of a top.

Description

technical field The invention relates to an accelerometer error calibration and compensation method, which can be applied to the error calibration and compensation of other inertial devices such as gyroscopes, and belongs to the fields of inertial device testing and inertial navigation. technical background The inertial navigation system has the characteristics of full autonomy, high concealment, high bandwidth, and continuous output. It has strategic significance in national defense and is one of the most important equipment in the fields of aviation, aerospace, and navigation. The performance of inertial devices (gyroscopes and accelerometers) is the most important factor affecting the accuracy of inertial navigation systems. 80% of inertial navigation system errors are caused by device errors. Therefore, improving the accuracy of inertial devices is the most important factor in the development of inertial technology. research content. There are often two ways to improve...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): G01P21/02
Inventor 徐烨烽杨国梁张仲毅李魁
Owner BEIHANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products