Position surveillance using one active ranging satellite and time of arrival of a signal from an independent satellite

• US 4,161,734 A
• Filed: 10/17/1977
• Issued: 07/17/1979
• Est. Priority Date: 10/17/1977
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: General Electric Company
• Inventors: Anderson, Roy E.
• Primary Examiner(s): Wilbur, Maynard R.
• Assistant Examiner(s): Goodwin, Lawrence
• Application Number:
  US05/842,401
• Time in Patent Office: 638 Days
• Field of Search: 343/112 R, 343/100 ST, 343/103, 343/6.5 R, 325/4
• US Class Current: 342/352
• CPC Class Codes: G01S 1/24 the synchronised signals being pulses or equivalent modulations on carrier waves and the transit times being compared by measuring the difference in arrival time of a significant part of the modulations , e.g. LORAN systems
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial
• CPC Class Codes: G01S 5/14 Determining absolute distances from a plurality of spaced points of known location

Abstract

The position of a ship or other object being located is determined at an earth station using an active ranging satellite and a satellite which transmits time signals. One line of position is determined by two-way active ranging through the first satellite. The other line of position is determined by one-way ranging from the second satellite. The time interval between the time of arrival of the timing signal at the ship and reception of the active ranging signal at the ship is measured and sent back to the earth station with the ship'"'"'s active ranging response. The position fix is then computed at the earth station.

Claims

1. A method of position surveillance using a plurality of satellites having known locations and including a first satellite that transmits timing signals, comprising the steps of

receiving at an object to be located and at a fixed earth station the timing signal transmitted by said first satellite,

performing a two-way active range measurement after reception of said first satellite timing signal at the earth station by transmitting an active ranging signal from the earth station through a second satellite to the object and back, to thereby derive the ranging time between said second satellite and object,

measuring the time of arrival of said first satellite timing signal at the object relative to reception of said active ranging signal at the object and deriving the elapsed time interval therebetween, and transmitting said elapsed time interval to the earth station,

computing at the earth station the position fix of said object from the known locations of said first and second satellites and earth station, the elapsed time interval measured at the object, and the ranging time between said second satellite and object, and displaying the position fix so obtained.

2. The method of claim 1 wherein the step of performing a two-way active range measurement comprises measuring at least the two-way ranging time between transmission and reception of said active ranging signal at the earth station, and wherein the elapsed time interval measured at the object is transmitted through said second satellite to the earth station following retransmission of said active ranging signal from the object through said second satellite to the earth station.

3. The method of claim 2 wherein the step of computing the position fix of said object comprises computing a first line of position of the object from the known location of said second satellite and the range from said second satellite to the object, and computing a second line of position of said object from the known location of said first satellite and the range from said first satellite to the object, the last-mentioned range being derived from the ranges to said first and second satellites from the earth station, the range from said second satellite to the object, and the elasped time interval measured at the object, and determining the position fix at the intersection of said first and second lines of position.

4. The method of claim 2 wherein said first satellite is a time distribution satellite transmitting said timing signals at precise regular intervals, and said active ranging signal has a time marker, and the step of measuring the time of arrival of said timing signal relative to reception of said active ranging signal at the object is comprised by starting and stopping a time interval counter with a sequentially received timing signal and ranging signal time marker.

5. The method of claim 1 further including a third satellite that transmits timing signals simultaneous with the transmission of timing signals from said first satellite, and further including the steps of receiving at the object the timing signal transmitted by said third satellite, measuring a second elapsed time interval between the time of arrival of said third satellite timing signal at the object and reception of said active ranging signal at the object, and transmitting said second elapsed time interval to the earth station.

6. A method of position surveillance using first and second satellites having known locations comprising the steps of

receiving at an object to be located and at a fixed earth station a timing signal transmitted by said first satellite,

performing a two-way active range measurement after reception of said timing signal at the earth station by transmitting an active ranging signal from the earth station through said second satellite to the object and back through said second satellite to the earth station, and measuring at least the two-way ranging time between transmission and reception of said active ranging signal at the earth station,

measuring the time of arrival of said timing signal at the object relative to reception of said active ranging signal at the object and deriving the elapsed time interval therebetween, and transmitting said elapsed time interval through said second satellite to the earth station, and

supplying at least the two-way ranging time, the elapsed time interval measured at the object, and data on the locations of said first and second satellites and earth station to a computer for computation of the position fix of the object to be located.

7. The method of claim 6 wherein said first satellite transmits timing signals at regular intervals and wherein said active ranging signal has a time marker, and the step of measuring the time of arrival of said timing signal relative to reception of said active ranging signal is comprised by starting and stopping a time interval counter with a sequentially received timing signal and ranging signal time marker.

8. The method of claim 6 wherein said first satellite is a time distribution satellite transmitting timing signals at precise regular intervals and said second satellite is an active ranging and communications satellite, and wherein said active ranging signal has a time marker, and the step of measuring the time of arrival of said timing signal relative to reception of said active ranging signal at the object is comprised by repeatedly starting a time interval counter with said timing signals at regular intervals and stopping said counter with the ranging signal time marker when an active ranging signal is received to thereby generate said elapsed time interval.

9. A method of position surveillance using a plurality of satellites having known locations and including a timing signal satellite that transmits timing signals at precisely known intervals, comprising the steps of

receiving at an object to be located and at a fixed earth station the timing signal transmitted by said timing signal satellite,

performing a two-way active range measurement in response to reception of said timing signal at the earth station by transmitting an active ranging signal through an active ranging satellite to the object and back through said active ranging satellite to the earth station, and measuring at least the two-way ranging time between transmission and reception of said active ranging signal at the earth station to thereby derive the range from said second satellite to the object,

measuring the time of arrival of said timing signal at the object relative to reception of said active ranging signal at the object and deriving the elapsed time interval therebetween, and transmitting the elapsed time interval through said active ranging satellite to the earth station,

computing a line of position of the object with respect to said active ranging satellite from the known locations of said earth station and active ranging satellite and the one-way ranging time from said active ranging satellite to the object,

computing a line of position of the object with respect to said timing signal satellite from the known locations of said active ranging and timing signal satellites and earth station, the elapsed time interval measured at the object, and the range from said active ranging satellite to the object,

determining the position fix of said object at the intersection of said lines of position, and displaying the position fix so obtained.

10. The method of claim 9 wherein the step of performing a two-way active range measurement comprises transmitting said active ranging signal after reception of said timing signal at the earth station, and wherein the step of transmitting the elapsed time interval measured at the object to the earth station is performed following retransmission of said active ranging signal from the object through the active ranging satellite to the earth station.

11. The method of claim 10 wherein said active ranging signal has a time marker, and the step of measuring the time of arrival of said timing signal relative to reception of said active ranging signal at the object is comprised by starting a time interval counter with said timing signal and stopping said counter with the ranging signal time marker to thereby generate said elapsed time interval.

12. The method of claim 10 wherein said timing signal satellite is a time distribution satellite transmitting timing signals at regular intervals, and said active ranging signal has a time marker, and the step of measuring the time of arrival of said timing signal relative to reception of said active ranging signal at the object is comprised by repeatedly starting a time interval counter with said timing signals at regular intervals and stopping said counter with the ranging signal time marker when said active ranging signal is received at the object to thereby generate said elapsed time interval.