DocumentCode
2999423
Title
A Fusion Estimation Method for Flight State Estimation
Author
Runquan, WANG ; Zhongke, Shi
Author_Institution
Coll. of Autom., Northwestern Polytech. Univ., Xi´´an, China
fYear
2010
fDate
25-27 June 2010
Firstpage
57
Lastpage
61
Abstract
To get accurate estimation of flight state, a new fusion estimation method was presented. In the scheme, equipments of INS, GPS, wireless radio, and infrared equipments with different wavelength were considered. Firstly, three dimensional motion model of an aircraft was described, and then model simplification was discussed. By analysis of deferent equipment measurement errors, a new method for equivalent computational measurements and equivalent error were proposed. The new method was used for flight data processing. The experimental results show that fusion estimation outperforms any single measurement.
Keywords
aircraft testing; inertial navigation; inertial systems; measurement errors; state estimation; GPS; INS; aircraft; flight data processing; flight state estimation; fusion estimation method; infrared equipments; measurement errors; three dimensional motion model; wireless radio; Aerodynamics; Aircraft; Measurement errors; Measurement uncertainty; Noise measurement; State estimation; flight state; fusion estimation; measurement errors;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical and Control Engineering (ICECE), 2010 International Conference on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-6880-5
Type
conf
DOI
10.1109/iCECE.2010.22
Filename
5630849
Link To Document