Pseudolite-based precise positioning system with synchronised pseudolites

• US 20050015198A1
• Filed: 11/06/2002
• Published: 01/20/2005
• Est. Priority Date: 11/06/2001
• Status: Abandoned Application

• Current Assignee: Chang-Don Kee
• Original Assignee: Chang-Don Kee
• Inventors: Yun, Doo-Hee, Kee, Chang-Don
• Application Number:
  US10/494,193
• Publication Number:
  US 20050015198A1
• Time in Patent Office: Days
• US Class Current: 701/207
• CPC Class Codes: G01S 1/20 using a comparison of transit time of synchronised signals transmitted from non-directional antennas or antenna systems spaced apart, i.e. path-difference systems
• CPC Class Codes: G01S 19/11 wherein the cooperating elements are pseudolites or satellite radio beacon positioning system signal repeaters
• CPC Class Codes: G01S 19/46 the supplementary measurement being of a radio-wave signal type

Abstract

Pseudolite-based precise positioning system with synchronised pseudolites that can compute the position of a mobile station with slave pseudolites synchronised to master pseudolite is provided. Therefore pseudolite-based precise positioning system according to present invention does not need correction information of a reference station. A pseudolite-based precise positioning system for computing the position of a mobile station without correction information of a reference station, the pseudolite-based precise positioning system includes: master pseudolite with reference clock of the positioning system; at least one slave pseudolite having digitally controlled numerical controlled oscillator means; mobile station computing the position of itself based on the clock-synchronised signal from the master pseudolite and the slave pseudolite without correction information of a reference station; and clock synchronisation loop filter means having the digitally controlled numerical controlled oscillator means synchronise the clock of the slave pseudolite to the clock of the master pseudolite by transmitting synchronisation information U k? of the slave pseudolite to the digitally controlled numerical controlled oscillator means, clock synchronisation loop filter means generating the synchronisation information U k? based on the pseudorange information and carrier phase information received from the master pseudolite and the slave pseudolite.

Claims

1. A precise navigation system using pseudolites that can determine a position of a mobile station even without correction information transmitted from a reference station through a data link, comprising:

a master pseudolite having a reference clock of the navigation system;

at least one slave pseudolite having a digitally controlled numerical controlled oscillating means;

a mobile station which determines a position of the mobile station based on a clock synchronized signal transmitted from the master and slave pseudolites even without correction information transmitted from the reference station through the data link; and

a clock synchronization loop filtering means for generating synchronization information U_k of the slave pseudolite(s) based on the pseudorange and/or carrier-phase information received from the master pseudolite and the slave pseudolite(s), and transmitting the synchronization information U_k to the digitally controlled numerical controlled oscillating means so that the digitally controlled numerical controlled oscillating means could synchronize the clock(s) of the slave pseudolite(s) with the reference clock of the master pseudolite.

2. The system as recited in claim 1, wherein the clock synchronization loop filtering means includes a processor, and the processor controls the clock synchronization loop filter to perform the steps of:

a) generating a single differenced pseudorange information and a single differenced carrier-phase information based on the pseudorange and/or carrier-phase information;

b) smoothing the received pseudorange using carrier-phase information and generating smoothed pseudorange; and

c) generating a controlled signal for controlling the digitally controlled numerical controlled oscillating means to synchronize the clock(s) of the slave pseudolite(s) with the reference clock of the master pseudolite gradually based on the smoothed pseudorange and/or carrier-phase information.

3. The system as recited in claim 2, where the step a) includes the steps of:

a1) computing a single differenced range measurement _mΔ

_sφ

between the master pseudolite and the slave pseudolite(s) based on Equation 1 below; and

a2) generating a clock synchronization error information _mΔ

_sb between the master pseudolite and the slave pseudolite(s) by using Equation 3 based on the single differenced range measurement _mΔ

_sφ

between the master pseudolite and the slave pseudolite(s) and geometrical distance difference information _mΔ

_sd between the reference station and the master and slave pseudolites, which is predetermined by using Equation 2,

_mΔ

_sφ

≡

φ

_m−

φ

_s 

 

Eq. 1
_mΔ

_sd≡

d_r^m−

d_r^s 

 

Eq. 2
_mΔ

_sb≡

b_m−

b_s=mΔ

_sφ

−

_mΔ

_sd 

 

Eq. 3

wherein _mΔ

_sφ

represents a single differenced range;

φ

_m denotes a carrier-phase of the master pseudolite;

φ

_s denotes a carrier-phase of the slave pseudolite;

_mΔ

_sd denotes a single differenced geometrical distance between the master pseudolite and the slave pseudolite;

d_r^m denotes a geometrical distance between the master pseudolite and the reference station;

d_r^s denotes a geometrical distance between the slave pseudolite and the reference station;

_mΔ

_sb denotes a clock synchronization error between the master pseudolite and the slave pseudolite;

b_m denotes a clock of the master pseudolite; and

b_s denotes a clock of the slave pseudolite.

4. The system as recited in claim 2, wherein the step c) includes the step of:

synchronizing the single differenced pseudorange between the master pseudolite and the slave pseudolite(s) with the single-differenced geometrical distance.

5. The system as recited in claim 2, wherein the step c) includes the step of:

synchronizing a frequency of the slave pseudolite(s) with a frequency of the master pseudolite based on a Doppler information of the master and slave pseudolites.

6. The system as recited in claim 2, wherein the step c) includes the step of:

synchronizing a carrier-phase of the slave pseudolite(s) with a carrier-phase of the master pseudolite based on the carrier-phases of the master and slave pseudolites.

7. The system as recited in claim 1, wherein the mobile station determines the position of the mobile station within a meter-unit error based on the pseudorange information.

8. The system as recited in claim 1, wherein the mobile station determines the position of the mobile station within a centimeter-unit error based on the carrier-phase information.

9. The system as recited in claim 1, wherein the master and slave pseudolites uses a frequency of Global Positioning System satellite navigation system.

10. The system as recited in claim 1, wherein the master and slave pseudolites use a clean and acquisition (C/A) code or a precision (P) code as a pseudo-random number (PRN) code.

11. The system as recited in claim 1, wherein the master and slave pseudolites use a PRN code having a rate of 1.023 MHz or 10.23 MHz.

12. The system as recited in claim 1, wherein said system is established in the indoors or the outdoors.

13. A precise navigation system using pseudolites that can determine a position of a mobile station even without correction information transmitted from a reference station through a data link, comprising:

a master pseudolite having a reference clock of the navigation system;

at least one slave pseudolite having a digitally controlled numerical controlled oscillating means connected to the master pseudolite though a cable or wireless data link and controls its clocks based on the reference clock transmitted from the master pseudolite; and

a mobile station which determines a position of the mobile station based on a clock synchronized signal transmitted from the master and slave pseudolites even without correction information transmitted from the reference station through the data link.