Title :
Application of extended Kalman filter in ultra-tight GPS/INS integration based on GPS software receiver
Author :
Yu, Jing ; Chen, Xiyuan
Author_Institution :
Key Lab. of Micro-Inertial Instrum. & Adv. Navig. Technol., Southeast Univ., Nanjing, China
Abstract :
When designing the ultra-tight GPS/INS integration, the architecture of Kalman filter is the key to its successful performance; the crux of this architecture is the measurement model. Aiming at the dependence of numbers of tracked GPS satellites and poor noise immunity in loose and tight integration modes, this paper proposes a new method of ultra-tight integration, using the Q(quadrature) signal from the GPS receiver correlator, receiver position and velocity to form the measurements of the extended Kalman filter. The experiments are carried out based on semi-physics, using the factual data solved by GPS software receiver, and the results show good performance.
Keywords :
Global Positioning System; Kalman filters; artificial satellites; inertial navigation; radio receivers; GPS satellites; GPS software receiver; GPS-INS integration; extended Kalman filter; noise immunity; quadrature signal; Application software; Global Positioning System; Instruments; Navigation; Position measurement; Q measurement; Satellites; Software performance; Tracking loops; Velocity measurement; Extended Kalman filter; GPS/INS; Ultra-tight integration;
Conference_Titel :
Green Circuits and Systems (ICGCS), 2010 International Conference on
Conference_Location :
Shanghai
Print_ISBN :
978-1-4244-6876-8
Electronic_ISBN :
978-1-4244-6877-5
DOI :
10.1109/ICGCS.2010.5543092