Skipping z-counts and accurate time in GPS receivers
View Patent ↗A navigation-satellite receiver comprises high-sensitivity radio frequency front-end and navigation processor associated with a client CPU. The client CPU runs an operating system that serially communicates with the navigation processor. The client CPU is also able to obtain navigation data system transmissions from a network server and provides such when the direct satellite signals in the high-sensitivity environment are too weak to be demodulated directly. A low power, low frequency oscillator with a watch-type crystal and counter are used as a real time clock to keep time uncertainty under fifty milliseconds when the receiver is hibernating. If the time uncertainty and position uncertainty are below certain maximums when the receiver is re-awakened, then a minimum number of satellites will be needed and making a preliminary z-count to each can be avoided.
1. A method for faster warm-starts of a high-sensitivity navigation satellite receiver in a weak signal environment, the method comprising:
during a first session with a GPS receiver, acquiring GPS satellites and producing a user position fix and solving GPS system time at a receiver millisecond interval;
reading and calibrating a count relative to said receiver millisecond interval from a crystal-oscillator driven timer included in said GPS receiver;
logging in a memory any count obtained from said timer and the GPS system time when the count was obtained;
powering down to end said first session and powering back up to begin a second session, all the while said timer is kept alive and continues to advance its count;
reading the count of said timer at a receiver millisecond interval and subtracting a last count stored in said memory in said first session to determine a turn-off period that the GPS receiver was turned-off; and
adding said turn-off period to a last known GPS system time to set the receiver time.
2. The method of claim 1 , further comprising:
testing a position uncertainty, and
if said position uncertainty exceeds approximately one-half a codephase ambiguity distance, then obtaining z-counts to three satellites to then reduce the uncertainty to under one-half the codephase ambiguity distance.
3. The method of claim 1 , further comprising:
checking if a time uncertainty is under ten seconds by reading the current timer count and adding the current timer count to a system time obtained in the step of calibrating, and if the time uncertainty is under ten seconds, determining a position fix without z-counts but acquiring at least four satellites.
4. The method of claim 1 , further comprising:
clocking said timer at about 32-KHz and operating it with a power dissipation of less than ten microwatts.