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
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;
Conference_Titel :
Electrical and Control Engineering (ICECE), 2010 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-6880-5
DOI :
10.1109/iCECE.2010.22