Title :
Estimate of the GPS block IIR AutoNav clock behavior
Author_Institution :
Aerosp. Corp., Los Angeles, CA, USA
Abstract :
The GPS Block IIR and Block ITF satellites will have an on-board capability to estimate clock and ephemeris parameters autonomously; this capability is referred as Autonomous Navigation (AutoNav). In the AutoNav mode, each GPS satellite makes pseudorange measurements to other visible satellites. The measurements and other mission data are crosslinked to other GPS satellites. This paper presents the estimated behavior of the three AutoNav dock errors: (1) an individual AutoNav satellite clock estimated error which is the difference between the individual clock error and its estimation by the AutoNav, (2) the AutoNav ensemble clock error which is the average of all the individual AutoNav clock estimated errors, (3) the AutoNav clock residual or synchronization error which is the difference between the AutoNav clock estimated error and the AutoNav ensemble clock error
Keywords :
Global Positioning System; IIR filters; Kalman filters; clocks; estimation theory; measurement errors; synchronisation; transfer standards; Autonomous Navigation; GPS satellite; IIR AutoNav clock; clock error; ephemeris parameters; estimated error; estimated errors; on-board capability; pseudorange measurements; residual error; synchronization error; Aging; Clocks; Equations; Error analysis; Estimation error; Frequency synchronization; Global Positioning System; Satellite constellations; Satellite navigation systems; Timing;
Conference_Titel :
Frequency and Time Forum, 1999 and the IEEE International Frequency Control Symposium, 1999., Proceedings of the 1999 Joint Meeting of the European
Conference_Location :
Besancon
Print_ISBN :
0-7803-5400-1
DOI :
10.1109/FREQ.1999.840761