Title :
GPS Aided Inertial Navigation
Author :
Nielson, John T. ; Swearingen, Gary W. ; Witsmeer, A.J.
Author_Institution :
Boeing Aerospace Company
fDate :
3/1/1986 12:00:00 AM
Abstract :
The Global Positioning System is an extremely accurate satellite-based navigation system which, after its completion in 1989, will provide users worldwide, 24 hour. all weather coverage. A joint research project among Boeing, Rockwell-Collins, and Northrop has been completed in which a GPS receiver was integrated with a low-cost strap-down inertial navigation system and a flight computer. A Kalman filter in the latter allows in-fight alignment and calibration of the INS. In addition, feedback from the INS to the GPS receiver improves the system´s ability to reacquire satellite signals after outages. The resulting system combines the accuracy of GPS with the jamming immunity and autonomy of inertial navigation. System tests were conducted in which a Boeing owned T-33 jet aircraft was flown through known test pattern to align and calibrate the INS. Earlier tests, including tests against an airborne jammer, were conducted in a modified passenger bus.
Keywords :
Aerospace electronics; Aircraft navigation; Clocks; Global Positioning System; Inertial navigation; Jamming; Position measurement; Redundancy; Satellites; Testing;
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE
DOI :
10.1109/MAES.1986.5005069