The Design of Numerical Control all Attitude Integrated Gyro Test Turntable

Qi Wang; Fan Yang; Xie Nong; Yun Ming Huang

doi:10.4028/www.scientific.net/AMR.898.530

Paper Titles

Modelling and Simulation of Inverse Kinematics for Planar 3-RRR Parallel Robot Based on SimMechanics
p.510

Neural Network Sliding Mode Control of 5DOFs Robotic Manipulator
p.514

Application Research of Numerical Control Machining Technology in Mechanical Manufacturing
p.521

Research on Automatic Correction Method for Cigarette Making Machine Transmission Device Based on Fuzzy-PID Dual Mode Control
p.525

The Design of Numerical Control all Attitude Integrated Gyro Test Turntable
p.530

PSO in Two-Wheeled Self-Balancing Robot Control Research
p.534

The Development of Control System for a Magnetorheological Finishing Prototype
p.538

The Development of Measurement and Control System for a Machine Tool
p.542

Dual Hydraulic Cylinders Synchronized Control Strategy
p.546

HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 898The Design of Numerical Control all Attitude...

The Design of Numerical Control all Attitude Integrated Gyro Test Turntable

Abstract:

This paper introduces the design points of the numerical control all attitude combined gyroscope test turntable. This Test table includes the course and pose angle given system, heading and attitude angle testing system and three weeks of servo system Heading and attitude angle of a given system using ZAZ1413 angle digital conversion module. Heading and attitude angle measurement system using SZZ1413 angle conversion module.

You might also be interested in these eBooks

Applied Material Science and Related Technologies

View Preview

Info:

Periodical:

Advanced Materials Research (Volume 898)

Pages:

530-533

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.898.530

Citation:

Cite this paper

Online since:

February 2014

Authors:

Qi Wang*, Fan Yang, Xie Nong, Yun Ming Huang

Keywords:

All Attitude Gyroscopes, Angle/Number, Number/Angle, Three Axis Servo System

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] SHEN X R, et al. Extended Kalman filter method for micro-interial strap down attitude determination system[j]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 3399(8): 933-935.

Google Scholar

[2] Kim S, Kim JH. Adaptive fuzzy-network-based c measure map-matching algorithm for car navigation system[J]. IEEE Trasactions on Industrial Electronics, 2001, 48(6): 432-441.

DOI: 10.1109/41.915423

Google Scholar

[3] Dellacherie S Burgaud L, di Crescenzo P. Improve-HDL-a Do-254 formal property checker used for design and verification of avionics protocol controller[A]. Proceedings of Digital Avionics Systems Conference[C], 2003, 1.A. 1-1, 1-8.

DOI: 10.1109/dasc.2003.1245801

Google Scholar

[4] Brotherton T, Luppold R, Padykula P, Wade R. Generic integrated PHM/controller system[A]. Proceedings of 2005 IEEE Aerospace Conference[C], 2005, 3427-3437.

DOI: 10.1109/aero.2005.1559645

Google Scholar

[5] Implementation of Military Configuration Management Syetems. LI Hua, LI Gang, CHEN Lin. Journal of Air Force Radar Academy. Mar. 2007, p.68–73.

Google Scholar

[6] Design of VXI-based General Testing Module. CHEN xiaohan, QUE peiwen. Computer Measurement &control. 2003; pp.968-969.

Google Scholar