Detection for Heading and Attitude Signal Conversion Equipment of Aircraft Based on Virtual Instrument Technology

Abstract:

Article Preview

The scheme adopts computer testing technology, virtual instrument and virtual system technology to realize the automatic detection for heading and attitude signal conversion equipment of aircraft. It greatly improves the test efficiency. Test time was reduced from 30 minutes to 3 minutes. Based on wavelet analysis and hierarchical decision, program module of connected line identification is design and it improves the reliability of program running. Noisy signals are de-noised by automatic zoom function of wavelet transform and that solves the interference problems of AC power supply.

Info:

Periodical:

Edited by:

Mohamed Othman

Pages:

1188-1191

Citation:

X. Y. Lv et al., "Detection for Heading and Attitude Signal Conversion Equipment of Aircraft Based on Virtual Instrument Technology", Applied Mechanics and Materials, Vols. 229-231, pp. 1188-1191, 2012

Online since:

November 2012

Export:

Price:

$38.00

[1] W.L. Lv and J.F. Wang. Measurement & Control Technology : The Essentials of Design for Aeronautical Test Equipments. Vol. 30( 2011), p.115.

[2] F.Y. Duan and L.M. Chang. Computer Measurement & Control: Study and Design on Synthetic Detector of Navigation Attitude System for a Certain Type Airplane. Vol. 14(2006), p.698.

[3] B.G. Zhou. Computer Measurement & Control: Design of Wavelet De-noising Instrument Based on Virtual Instrument Technology. Vol. 17(2009), p.794.

[4] D.F. Jiang, M. Cheng. Chinese Journal of Scientific Instrument: A Real-time Wavelet De-noising Algorithm. [J]. Vol. 25(2004), p.781.