Title :
Multipath-adaptive GPS/INS receiver
Author :
Erickson, John W. ; Maybeck, Peter S. ; Raquet, John F.
Author_Institution :
Dept. of Electr. & Comput. Eng., Air Force Inst. of Technol., Wright-Patterson AFB, OH, USA
fDate :
4/1/2005 12:00:00 AM
Abstract :
Multipath interference is one of the contributing sources of errors in precise global positioning system (GPS) position determination. This paper identifies key parameters of a multipath signal, focusing on estimating them accurately in order to mitigate multipath effects. Multiple model adaptive estimation (MMAE) techniques are applied to an inertial navigation system (INS)-coupled GPS receiver, based on a federated (distributed) Kalman filter design, to estimate the desired multipath parameters. The system configuration is one in which a GPS receiver and an INS are integrated together at the level of the in-phase and quadrature phase (I and Q) signals, rather than at the level of pseudo-range signals or navigation solutions. The system model of the MMAE is presented and the elemental Kalman filter design is examined. Different parameter search spaces are examined for accurate multipath parameter identification. The resulting GPS/INS receiver designs are validated through computer simulation of a user receiving signals from GPS satellites with multipath signal interference present The designed adaptive receiver provides pseudo-range estimates that are corrected for the effects of multipath interference, resulting in an integrated system that performs well with or without multipath interference present.
Keywords :
Global Positioning System; Kalman filters; adaptive estimation; inertial navigation; interference (signal); radio receivers; GPS position determination; distributed Kalman filter design; federated filter; global positioning system; inertial navigation system; multipath interference; multipath parameter identification; multipath signal estimation; multipath-adaptive GPS/INS receiver; multiple model adaptive estimation; parameter search spaces; Adaptive estimation; Antennas and propagation; Computer errors; Global Positioning System; Inertial navigation; Interference; Parameter estimation; Receiving antennas; Satellites; Transmitters;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.2005.1468754