Position-fixing system

• US 4,613,864 A
• Filed: 01/16/1984
• Issued: 09/23/1986
• Est. Priority Date: 01/19/1983
• Status: Expired due to Fees

• Current Assignee: Alcatel SA (Nokia Corporation)
• Original Assignee: International Standard Electric Corporation (ITT, Inc.)
• Inventors: Hofgen, Gunter
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Issing, Gregory C.
• Application Number:
  US06/571,012
• Time in Patent Office: 981 Days
• Field of Search: 343/356, 343/357, 343/387, 343/465, 343/463, 343/450, 343/352, 343/458, 364/449
• US Class Current: 342/357.22
• CPC Class Codes: G01S 13/876 Combination of several spaced transponders or reflectors of known location for determining the position of a receiver G01S13/874 takes precedence
• CPC Class Codes: G01S 19/01 Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
• CPC Class Codes: G01S 19/42 Determining position

Abstract

Several satellites serving as reference stations (S_j) for a user revolve about the earth in different orbits. At least four reference stations must be within sight of a user station (N) at the same time. The user station measures the ranges to at least four reference stations by one-way ranging. From these ranges and the positions of the reference stations, which are transmitted as data words, the user station determines its position.

To determine the positions of the reference stations, the ranges from the respective reference station to at least three ground stations (B_i) are measured by two-way ranging. From these ranges and the known positions of the ground stations, the position of the reference station is obtained. The interrogation signals of all reference stations contain the same basic signal (K_s), which represents a pseudorandom code. The reply signals of the ground stations contain differently coded signals (K_Bi), so that the ground stations are identifiable with the aid of the codes assigned to them. If the interrogation and reply signals contain the times of transmission (t_j) and arrival (t_i), respectively, of the interrogation signal, and the signal transit times are measured, the clocks of the reference stations and of the ground stations can be synchronized.

Claims

1. A position-fixing system wherein a user station (N) determines its position from the ranges to and the positions of several reference stations (S_j) carried by satellites, the ranges being measured by one-way ranging, and wherein the signals used for position-fixing purposes are radio-frequency signals, characterized in that the reference stations (S_j) are controlled so that only one of the reference stations within sight of the user station is active at any given time, that the ranges from each of several ground stations (B_i) to each reference station (S_j) are measured by a two-way ranging method, wherein an interrogator station, the reference station or the ground station, transmits interrogation signals while a transponder station, the ground station or the reference station, transmits reply signals, and that the position of a reference station is defined by the intersection of spheres having their centers at the ground stations, the radii of the spheres being the ranges from the respective ground station to the respective reference station and further characterized in that the interrogation signals and the reply signals each consist of two parts (FIG. 2) the first of which is a synchronization preamble (SY), and the second of which indicates when the interrogation signal was transmitted (t_j) from the interrogator station and received (t_i) by the transponder station, respectively.

2. A position-fixing system as claimed in claim 1, characterized in that the position of a reference station is determined at said reference station, and that the position data are transmitted to the user station.

3. A position-fixing system as claimed in claim 1, characterized in that the measured ranges from the ground station to the reference station, or signal transit times from which the ranges can be determined are transmitted to the user station, and that the positions of the reference stations are determined at the user station.

4. A position-fixing system as claimed in claim 1 characterized in that the interrogation and reply signals of a sequence of like basic signals (K_s, K_Bi) each forming a pseudorandom code.

5. A position-fixing system as claimed in claim 4 characterized in that the basic signals (K_s) are the same for all reference stations, and that each ground station is assigned an individual basic signal (K_Bi), so that the ground stations can be identified with the aid of the basic signals transmitted by them.

6. A position-fixing system as claimed in claim 1 characterized in that the signal transit times between the interrogator and transponder stations and the transmitted times are used to synchronize the clocks at the reference stations.

7. A position-fixing system as claimed in claim 6, characterized in that a correcting value or correcting the clock at the ground station is derived from the distance between a reference station and a ground station, the instants at which the reference station transmits a signal and at which the ground station receives this signal, and the delay of this signal in the ground station.

8. A position-fixing system as claimed in claim 1, characterized in that the Doppler shift (f_D) of the received signal is determined at each of the ground stations, and that the frequency of the signal transmitted from the ground station is shifted by the inverse Doppler shift with respect to the nominal transmission frequency.