Attitude measurement using a GPS receiver with two closely-spaced antennas

作者: Robert Pinto , James Kain

DOI:

关键词:

摘要: A system determines three-dimensional attitude of a moving platform using signals from two closely spaced Global Positioning System (GPS) antennas. The includes three rate gyroscopes and accelerometers rigidly mounted in fixed relationship to the aid determining attitude. applies one GPS antennas sufficient channels receiver support navigation. second additional receive interferometry. resolves ambiguity normally associated with interferometric heading solution by having antennas, uses interferometry refine coarse estimate plus Inertial Measurement Unit (IMU) transfer alignment solution. achieves sub-meter spacing merging many temporal measurements memory provided IMU time-history

参考文章(28)
Demoz Gebre-Egziabher, J. David Powell, Matt Schwall, Roger C. Hayward, John Wilson, Inertially Aided GPS Based Attitude Heading Reference System (AHRS) for General Aviation Aircraft Proceedings of the 1997 10th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GPS-97. Part 1 (of 2). pp. 289- 298 ,(1997)
David F. Hartman, Yeong-Wei A. Wu, Mark Youhanaie, FLIR boresight alignment ,(1996)
Debra L. Diefes, Leopold C. Fan, Charles E. Rodgers, Satellite location and pointing system for use with global positioning system ,(1993)
Debra L. Diefes, Leopold C. Fan, Charles E. Rodgers, Attitude determining system for use with global positioning system ,(1993)
Fred Robbins, Robert Yee, Inertial pointing and positioning system ,(1996)