Radio navigation system

• US 5,132,695 A
• Filed: 01/24/1991
• Issued: 07/21/1992
• Est. Priority Date: 02/01/1988
• Status: Expired due to Fees

• Current Assignee: Thomson-CSF (Thales SA)
• Original Assignee: Thomson-CSF (Thales SA)
• Inventors: Dumas, Bernard, Robin, Leon P.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US07/645,314
• Time in Patent Office: 544 Days
• Field of Search: 342/457, 342/451, 342/461, 364/458
• US Class Current: 342/461
• CPC Class Codes: G01S 11/08 using synchronised clocks
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 19/39 the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO

Abstract

A radio navigation system including:

a means to determine, at a point (M₁) of the trajectory of a moving body to be localized, the speed vector of said moving body and, possible, the "n" order derivatives of said speed vector (with n>1),

a means to perform at least three successive measurements of distance, respective between a geodesic point at the ground and three successive positions (M₁, M₂, M₃) of said moving body,

a means to computer the position (M₃) of said moving body by resolving a system of equations from the results thus obtained, expressed in one and the same reference system.

Claims

1. A radio navigation system comprising:

means to determine, at a point (M₁) of the trajectory of a moving body to be localized the speed vector of said moving body and the "n" order derivatives of said speed vector (with n>

1);

means including an interrogator-responder set to perform at least three successive measurements of distance in real time with respect to a single reference, respectively between a geodesic point at the ground where said responder is located and three successive positions (M₁, M₂, M₃) of said moving body, by measuring the time between interrogations made by said moving body and the responses of said responder;

means to compute the position (M₃) of said moving body by resolving a system of equations from the results thus obtained, expressed in said single reference system.

2. A system according to claim 1, wherein the means to determine said speed vector and the "n" order derivatives of said vector comprise a gyroscopic unit placed aboard said moving body.

3. A system according to claim 1, wherein the means to determine said speed vector and the "n" order

of said vector, comprises means to estimate the cartesian coordinates of said moving body on the basis of previous position measurements of said moving body, done in a global type of radio navigation system.

4. A system according to claim 3, wherein said global type radio navigation system consists of the GPS system, said moving body being fitted with an GPS receiver.

5. A system according to claim 1, wherein said means to perform distance measurements comprise an Trident interrogator-responder set, said interrogator being placed on board said moving body and said responder at said geodesic point on the ground.

6. A system according to claim 5, wherein said geodesic point on the ground is also fitted out with a GPS receiver in order to set up a differential GPS system which outputs differentiate information and wherein means to transmit the said differential information thus obtained are provided between said geodesic point on the ground and said moving body.

7. A system according to claim 6, wherein said means to perform distance measurements comprise a Trident interrogator-responder set, said interrogator being placed on board said moving body and said responder at said geodesic point on the ground, and wherein the transmission of said differential information is limited to a particular working mode of said Trident responder.

8. A system according to claim 6, wherein said means to perform distance measurements comprise a Trident interrogator-responder set, said interrogator being placed on board said moving body and said responder at said geodesic point on the ground, and wherein the reception of said differential information is done by means of a data reception channel integrated into said Trident interrogator-receiver.