Attitude Solution for Carrier Based on Quaternion Differential Equation of Picard Solver

Zhi Yang Gou; Lai Wei Jiang; Sheng Hong Fan; Chang Ru Liu; Qiang Wang

doi:10.4028/www.scientific.net/AMM.475-476.1572

Paper Titles

Applications of Multi-Point Mirror Supporting
p.1555

Study on Dynamic Behavior of Ancient Timber Structures Roof
p.1559

Reduce the Impact of Dynamic Strength of Concrete under Fire Conditions on Bearing Capacity of Reinforced Concrete Columns
p.1563

Numerical Simulation of Atmospheric Pressure Glow Discharges in Coaxial Tube
p.1567

Attitude Solution for Carrier Based on Quaternion Differential Equation of Picard Solver
p.1572

Oscillation for Third-Order Nonlinear Delay Dynamic Equations on Time Scales
p.1578

Study on Average Support Probability Oriented to Electromechanical Integration System
p.1583

Analyzing Tree Dynamic Modeling under Outdoors Environment
p.1588

Study on Bioinformatics with Dynamic Characteristics Change of the Hippocampal Neuron Model Caused by the Alzheimer Disease
p.1592

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 475-476Attitude Solution for Carrier Based on Quaternion...

Attitude Solution for Carrier Based on Quaternion Differential Equation of Picard Solver

Abstract:

The attitude information is indispensable to realize the full range of navigation part. Besides, in aerial remote sensing, photogrammetry and laser scanning, we can get exterior orientation elements by attitude of device. Based on Picard solving quaternion differential equation realized the real-time dynamic attitude matrix updating and attitude solution. Comparison of IMU three axis output, calculation error of heading is 0.036183°, pitch is 0.007969° and roll is 0.009627°. Finally, verify the feasibility and stability of Picard solving attitude.

You might also be interested in these eBooks

Sensors, Measurement and Intelligent Materials II

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 475-476)

Pages:

1572-1577

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.475-476.1572

Citation:

Cite this paper

Online since:

December 2013

Authors:

Zhi Yang Gou*, Lai Wei Jiang, Sheng Hong Fan, Chang Ru Liu, Qiang Wang

Keywords:

Attitude Matrix, Coordinate Rotation, Differential Equations, Quaternion Updates

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Titterton D.H.; Weston J.L. Srrapdown Intertial Navigation Technology, 2nd ed.; The Institution of Electrical Engineers: Hertfordshire, HK, (2004).

Google Scholar

[2] David H. Titterton, John L. Weston. Strapdown: Inertial Navigation Technology. Published by The IEE, (2004).

Google Scholar

[3] Zhang R. H, Jia H. G and Chen T: Optics and precision Engineering, 2008, 16(10), 1963-1970. (in Chinese).

Google Scholar

[4] Qin Y. Y: Inertial navigation. Science Press, 2005. (in Chinese).

Google Scholar

[5] Wang W. P, Yang B and Li F: Aerospace Control, 2012, 30 (3), 3-6. (in Chinese).

Google Scholar

[6] Shao Y. M: Northwestern Polytechnical University, 2007. (in Chinese).

Google Scholar

[7] Zhao X, Wang S. C and Yang D. F: Journal of Chinese Inertial Technology, 2011, 19(2), 163-169. (in Chinese).

Google Scholar

[8] DU H. L, Zhang R. H and Liu P: Optics and Precision Engineering, 2008, 16(10), 1956-1961. (in Chinese).

Google Scholar

[9] Gu H. Q: Nanjing University of Science and Technology, 2009. (in Chinese).

Google Scholar

[10] Jared B. Bancroft, Gerard Lachapelle:. Sensors, 2011, 11, 6771-6798.

Google Scholar

[11] Wei C. L, Zhang H. Y: Chinese Journal of Aeronautics, 2001, 14(3): 166-170. (in Chinese).

Google Scholar

[12] Yu J, Chen X. Y: Instrument Society Symposium, Jiangsu Province in 2010. (in Chinese).

Google Scholar

[13] R.E. Kalman. Maryland: Res- earch Institude for Advanced Study, (1960).

Google Scholar

[14] Yang Y, Hou X. L and Zhang Y: Journal Northwestern Polytechnical University, 2011, 29(5): 685 -688, (in Chinese).

Google Scholar