DocumentCode
2230533
Title
The Accuracy Relative Position Algorithm For Multi-Aircrafts
Author
Jiang, Tao ; Chen, Weidong
Author_Institution
Dept. of Electron. Eng. & Inf. Sci., Univ. of Sci. & Technol. of China, Hefei, China
fYear
2009
fDate
26-28 Dec. 2009
Firstpage
3864
Lastpage
3867
Abstract
For the applications of aircrafts work in collaboration, the initial relative position of multi-aircrafts is significant. A new method, achieved the relative position of aircrafts, is presented. Firstly, the multiple hypothesis is established, based on the error model of INS, to estimate the relative error covariance matrix between Inertial Navigation System(INS) information of multi-aircrafts, which is necessary for the least-square estimate method. Then the different least-square estimate results of the relative position between aircrafts can be obtained under each hypothesis. Finally, the weighted estimate results can be acquired according to the Bayes´s formula. Simulation results show the stabilization and the precision of this algorithm in the relative position.
Keywords
aircraft navigation; covariance matrices; inertial navigation; least mean squares methods; Bayes´s formula; accuracy relative position algorithm; inertial navigation system information; least-square estimate method; multi-aircrafts; multiple hypothesis; Aerospace electronics; Aerospace engineering; Aircraft manufacture; Aircraft navigation; Aircraft propulsion; Collaborative work; Computer errors; Dead reckoning; Inertial navigation; Information science;
fLanguage
English
Publisher
ieee
Conference_Titel
Information Science and Engineering (ICISE), 2009 1st International Conference on
Conference_Location
Nanjing
Print_ISBN
978-1-4244-4909-5
Type
conf
DOI
10.1109/ICISE.2009.1166
Filename
5455442
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