Study on Optimization of Samples by Rotation Vector Method Based on Attitude Calculating

Ye Du; Shun Shan Feng; Da Wei Yuan

doi:10.4028/www.scientific.net/AMR.482-484.26

Paper Titles

The Output Researching of a Cascaded Multilevel Class-D Power Amplifier
p.3

Research on TPL Cloud Service Platform Architecture
p.11

Numerical Simulation of 2D Hydraulic Jump Flow in a Vertical Plane
p.16

Empirical Analysis of the Relationship between World Class Manufacturing Practises and Enterprise Performance: Comparing Developing Countries with Developed Countries
p.21

Study on Optimization of Samples by Rotation Vector Method Based on Attitude Calculating
p.26

A BP Neural Network-Based Automatic Windshield Wiper Controller
p.31

Analysis on Engine Stall Issue of Closed Hydraulic System
p.35

Security Research of Messaging Middleware JMS-Based
p.39

FEM Analysis on the Phenomenon of Bilayer Nanofilm Bending into Nanotube with Effects of Adsorption and Temperature
p.43

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 482-484Study on Optimization of Samples by Rotation...

Study on Optimization of Samples by Rotation Vector Method Based on Attitude Calculating

Abstract:

According to mathematical model of MEMS, In case attitude updating period sampling period are the same , single-sample, two-sample and three-sample algorithm are studied based on rotation vector method, and the simulation and comparative analysis are proceed. In the same sample rate cases, the results show that calculating precision of two-sample and three-sample changes with growing attitude updating cycle. Before turntable test or practical application, all samples should be simulated respectively. Choose the best method for attitude solving and provides the basis for the engineering.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 482-484)

Pages:

26-30

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.482-484.26

Citation:

Cite this paper

Online since:

February 2012

Authors:

Ye Du, Shun Shan Feng, Da Wei Yuan

Keywords:

Attitude Updating, Rotation Vector, Sampling Rate

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Yongyuan Qin. Inertial navigation. Beijign,Science press. 2006(In Chinese)

Google Scholar

[2] Manjuan Zhou. The Research for the Laser Gyro Strapdown Explicit Guidance System. Missiles and Space Vehicles. 2001.(05):15-19. (In Chinese)

Google Scholar

[3] Tao Pan. Technology on low cost SINS/GPS integrated navigation system. Master's degree thesis from Institute of technology of nanjing university. 2004.10. (In Chinese)

Google Scholar

[4] Na LI; Weidong LIU; Hao ZHANG; Jian ZHU. Study of Strapdown Navigation Attitude Algorithms for Angular Rate Input. Journal of Projectiles Rockets Missiles and Guidance. 2006, 25(4):6-8. (In Chinese)

Google Scholar

[5] Bortz J.E .A new mathematical formulation for strap-down inertial navigation [J] . IEEE Transactions on Aerospace and Electronic Systems, 1971.7(1)：61~66

DOI: 10.1109/taes.1971.310252

Google Scholar

[6] Xu Han. The Techology of Attitude and Heading Algorithm and Data Acquisition in Strapdown Navigation System. Master's degree thesis from Harbin engineering university. 2005.2. (In Chinese)

Google Scholar