System and method for fast initialization of navigational satellite signal receivers
View Patent ↗The present invention provides a method and apparatus for a satellite navigation receiver to lock onto satellite signals in the cold start mode with no information on the receiver position, the satellite position, or time estimates stored in the receiver's memory. All satellites in a positioning system are divided into groups based on the satellite constellation structure. In an embodiment, the positioning system is the Global Positioning System (GPS) and all GPS satellites are divided into three groups. During initialization of the receiver, the satellites are searched per group to lock onto at least one satellite signal. Other satellites are then searched in a given order based on their respective distance or proximity to the first satellite acquired. This method reduces the Time-to-First-Fix (TTFF) ordinarily required by conventional receivers in the cold start mode.
1. A method of reducing initialization time of a satellite signal receiver, comprising the steps of:
dividing navigational satellites of a positioning system into a plurality of groups such that each group has a fixed number of said navigational satellites uniformly distributed over entire surface of Earth; and
configuring said receiver such that said receiver searches for navigational satellite signals per group in an assigned order to acquire a first satellite signal;
generating a two-dimensional (2D) matrix based on slot and plane of each of said navigational satellites; wherein
each row of said matrix contains unique identifiers of said navigational satellites; wherein each row has a target satellite; and wherein
each row is sorted by distance or proximity of each remaining navigational satellite in relation to said target satellite;
acquiring additional navigation satellite signals;
computing receiver position using the acquired first and additional satellite signals; and
displaying the computed receiver position.
2. The method of claim 1 , wherein
said groups comprises a first group, a second group, and a third group.
3. The method of claim 2 , wherein
said first group and said second group each has 12 navigational satellites.
4. The method of claim 1 , further comprising the step of:
selecting two navigational satellites from each orbit plane.
5. The method of claim 1 , wherein
each of said unique identifiers is a pseudo random noise (PRN) number uniquely identifying one of said navigational satellites.
6. The method of claim 1 , further comprising the step of:
determining said distance or proximity based on statistics of positions of said navigational satellites within an orbital period.
7. The method of claim 6 , wherein said orbital period is 11 hours 58 minutes.
8. The method of claim 6 , further comprising the step of:
determining an average distance or proximity of each remaining navigational satellite from the target satellite within the orbital period; and
for each row, sorting each remaining navigational satellite according to its average distance or proximity from the target satellite within the orbital period.
9. The method of claim 6 , further comprising the step of:
assigning a score to each remaining navigational satellite based on distances of the navigational satellites from the target satellite within the orbital period;
for each row, sorting each remaining navigational satellite according to its assigned score.
10. The method of claim 1 , further comprising the step of:
selecting twelve of said navigational satellites from said matrix after said first satellite signal is acquired.
11. The method of claim 1 , further comprising the step of:
locating a target satellite in the matrix whose unique identifier matches that of said first satellite signal acquired by the receiver; and
selecting first twelve navigational satellites from a row containing said matched unique identifier.
12. The method of claim 11 , further comprising the step of:
searching navigational satellites that follow said first twelve navigational satellites and that are within said row.
13. The method of claim 11 , wherein
said positioning system is a global positioning (GPS), Global'naya Navigatsionnaya Sputnikovaya Sistema (GLONASS), an European satellite navigation system (GALILEO) system, or a combination thereof.
14. A method of initializing a satellite signal receiver, comprising the steps of:
searching a first group of twelve navigational satellites uniformly distributed over entire surface of Earth;
acquiring a first navigational satellite signal from said first group; and acquiring remaining navigational satellite signals based on a two-dimensional matrix containing identification and statistical information of all navigational satellites of a positioning system, wherein
each row of said matrix contains unique identifiers of said navigational satellites;
each row has a target satellite; and
each row is sorted by distance or proximity of each non-target navigational satellite in relation to said target satellite;
computing receiver position using the acquired first and remaining satellite signals; and displaying the computed receiver position.
15. The method of claim 14 , wherein
each of said unique identifiers is a pseudo random noise (PRN) number uniquely identifying one of said navigational satellites.
16. The method of claim 14 , wherein
said positioning system is a global positioning (GPS), Global'naya Navigatsionnaya Sputnikovaya Sistema (GLONASS), an European satellite navigation system (GALILEO) system, or a combination thereof.
17. A method of initializing a satellite signal receiver, comprising the steps of:
searching a first group of twelve navigational satellites uniformly distributed over entire surface of Earth;
acquiring a first navigational satellite signal from said first group; and acquiring remaining navigational satellite signals based on a two-dimensional matrix containing identification and statistical information of all navigational satellites of a positioning system, wherein said distance or proximity is determined based on statistics of positions of said navigational satellites during an orbital period;
computing receiver position using the acquired first and remaining satellite signals; and
displaying the computed receiver position.
18. The method of claim 17 , wherein said orbital period is 11 hours 58 minutes.
19. A method of initializing a satellite signal receiver, comprising the steps of:
searching a first group of twelve navigational satellites uniformly distributed over entire surface of Earth;
acquiring a first navigational satellite signal from said first group; and acquiring remaining navigational satellite signals based on a two-dimensional matrix containing identification and statistical information of all navigational satellites of a positioning system;
computing receiver position using the acquired first and remaining satellite signals; and displaying the computed receiver position;
wherein if no navigational satellite signal is acquired from said first group, further comprising the step of:
searching a second group of twelve navigational satellites uniformly distributed over entire surface of Earth; and
acquiring said first navigational satellite signal from said second group.