Simulation of Accurate Navigation Technology for Aircraft Landing Approach

Ang Tai Li; Xiao Jiao Ma

doi:10.4028/www.scientific.net/AMM.329.406

Paper Titles

Charge-Sensitivity-Oriented Analysis of Quantum Point Contact Sensor Based on the Landauer's Formula
p.387

Design of Electrical Impedance Tomography System Based on Layer Stripping Process
p.392

The Hardware System of Rotational Electrical Impedance Tomography
p.397

Experimental Research on the Laser Scattering Properties of Smoke Particles
p.401

Simulation of Accurate Navigation Technology for Aircraft Landing Approach
p.406

Long-Term Wind Power Prediction Based on Rough Set
p.411

A Low-IF 2.4 GHz Integrated RF Receiver for Bluetooth Applications
p.416

Design of Single-Phase Active Power Filter
p.421

Research on the Gray Balance of Ink-Jet Printing Based on G7
p.429

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 329Simulation of Accurate Navigation Technology for...

Simulation of Accurate Navigation Technology for Aircraft Landing Approach

Abstract:

The purpose of this paper is to find a solid application and improve the integrated navigation system of aircraft independent landing. The main researches are focused on the issue how to improve the accuracy and reliability of the integrated navigation system, by means of the detailed analyzing about information fusion, and investigating accurate navigation technology for independent landing approach of aircraft. Next, the integrated navigation system models SINS/DGPS/TAN/ILS based on Federated filter are established, and the accurate navigation algorithm of landing is also researched. At the end, the paper gives its simulation results for independent lading approach, which show this algorithm is able to greatly improve the accuracy of speed and location information for aircraft accurate landing.

You might also be interested in these eBooks

Advanced Technologies on Measure and Diagnosis, Manufacturing Systems and Environment Engineering

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 329)

Pages:

406-410

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.329.406

Citation:

Cite this paper

Online since:

June 2013

Authors:

Ang Tai Li, Xiao Jiao Ma

Keywords:

Aircraft Landing Simulation, Data Fusion Algorithm, Filter Technology, Integrated Navigation Technology

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] J. Li, X. Li, K. Qian, GPS/SINS/Vision integrated navigation system for UAV, Journal of Chinese Inertial Technology, Vol.19, No.4, pp.457-461, Aug. (2011)

Google Scholar

[2] X. Chen, J.Yu, M. Gu, Study on tightly-coupled GPS/SINS integrated navigation system by using software GPS receiver, Proceedings of the IEEE Instrumentation and measurement Technology Conference, Hangzhou, China, pp.1-4, (2011)

DOI: 10.1109/imtc.2011.5944155

Google Scholar

[3] N. Aboelmaged, E. Ahmed, B.Mohamed, GPS/INS integration utilizing dynamic neural networks for vehicular navigation, Information Fusion, Vol.12, No.1, pp.48-57, (2011)

DOI: 10.1016/j.inffus.2010.01.003

Google Scholar

[4] N.A. Carlson, Federated filter for fault-tolerant integrated navigation systems, Proceedings of IEEE Position Location and Navigation Symposium, (1988)

DOI: 10.1109/plans.1988.195473

Google Scholar

[5] M. R. Javdan, R. J. Richards, Decentralized control systems theory a critical evaluation, International Journal of Control, Vol.26, No.1, pp.129-144, Jul., (1977)

DOI: 10.1080/00207177708922295

Google Scholar

[6] M. Adam, J. Fosbury, L. Crassidis, Relative navigation of air vehicles, Journal of Guidance, Control, and Dynamics, Vol. 31, No.4, pp.824-834, (2008)

DOI: 10.2514/1.33698

Google Scholar