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.
Simulation of Accurate Navigation Technology for Aircraft Landing Approach
Applied Mechanics and Materials ; 329 ; 406-410
2013-06-27
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Simulation of Accurate Navigation Technology for Aircraft Landing Approach
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