Automated repeating sextant (ARS)

• US 5,161,242 A
• Filed: 01/24/1989
• Issued: 11/03/1992
• Est. Priority Date: 01/24/1989
• Status: Expired due to Fees

• Current Assignee: Peter C. Boulay
• Original Assignee: Peter C. Boulay
• Inventors: Boulay, Peter C.
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Cosimano, Edward R.
• Application Number:
  US07/300,842
• Time in Patent Office: 1,379 Days
• Field of Search: 33/1 SC, 33/268, 33/281, 33/282, 33/, 356/141, 356/145, 356/146, 356/147, 364/455, 364/443
• US Class Current: 701/222
• CPC Class Codes: G01C 1/10 including an artificial horizon G01C1/14 takes precedence
• CPC Class Codes: G01S 3/786 the desired condition being maintained automatically
• CPC Class Codes: G01S 5/08 Position of single direction-finder fixed by determining direction of a plurality of spaced sources of known location

Abstract

The automated repeating sextant (ARS) is a navigational instrument suitable for air, sea and land use. The ARS uses an electronic artificial horizon, an A/D conversion board and either microchips or a computer, with software, to read a celestial body'"'"'s altitude above the horizon repeatedly in a brief period of time, and then compute a line of position from a statistically enhanced mean altitude; after a second or any successive line of position has been obtained the instrument either provides the latitude and longitude of the navigator, or combines the latitude and longitude with a graphic portrayal of the position on a simplified grid map. The instrument averages numerous individual observations and is relatively small, light and fast. The ARS may be embodied in a fully automated, continually-operating mode with a micro-computer, or may be embodied in a handheld version that is switched on and off. The body sighted by the ARS may be either a natural celestial body (sun, moon, navigational planet or navigational star) using light wave signals, or an artificial celestial body (manmade satellite), using radio frequency signals.

Claims

1. An automated, repeating sextant comprising:

means for receiving a signal from a celestial body;

means for measuring movement of the sextant about a first axis as a first signal which establishes an artificial horizon;

means for detecting a signal received from a celestial body and an angle of incidence of the received signal on the detecting means, said angle of incidence being output by said detecting means;

means responsive to plural values of said first signal and said angle of incidence for determining a mean altitude of the celestial body, and determining a line of position using said mean altitude and stored data ephemerides for the celestial body; and

,

means for displaying the line of position.

2. Repeating sextant according to claim 1, wherein said receiving means is a lens contained within a protective globe.

3. Repeating sextant according to claim 1, wherein said means for displaying is a digitized map of a given geographical area, and said line of position is placed over said map.

4. Repeating sextant according to claim 1, wherein said means for displaying is a video display terminal.

5. Repeating sextant according to claim 1, wherein said means for displaying is a liquid crystal display.

6. Repeating sextant according to claim 1, wherein said means for displaying is a light emitting diode display.

7. Repeating sextant according to claim 1, wherein said determining means further includes means for providing an updated date and time from which a mean time of a given observation of the celestial body during said line of position determination is derived.

8. Repeating sextant according to claim 1, wherein all information required to display a line of position is determined automatically.

9. Repeating sextant according to claim 1, wherein a line of position is determined for at least two different celestial bodies to provide a position fix of the sextant, said position fix being displayed on said displaying means.

10. Repeating sextant according to claim 1, wherein said mean altitude is statistically enhanced.

11. Repeating sextant according to claim 1, wherein said receiving means is a loop antenna.

12. Repeating sextant according to claim 11, wherein said celestial body is a manmade satellite which emits a radio frequency signal, and said detecting means is a radio frequency receiver which detects an angle of incidence of the radio frequency signal received by said loop antenna from said manmade satellite to determine an azimuth of said manmade satellite.

13. Repeating sextant according to claim 1, further including means for measuring roll of the sextant about a second axis, perpendicular to said first axis, as a second signal.

14. A repeating sextant according to claim 13, wherein said first and second signals are analog signals, said sextant further including means for converting said first and second signals to digital signals for input to said altitude and line of position determining means.

15. Repeating sextant according to claim 13, wherein said detecting means further detects a magnitude of said received signal to assist in identifying said celestial body, said magnitude being input to said determining means for deriving a calculated altitude of the celestial body from said stored data ephemerides.

16. Repeating sextant according to claim 15, wherein said calculated altitude is determined by applying stored Chebyshev formulae to said stored data ephemerides.

17. Repeating sextant according to claim 15, wherein said detecting means further includes an array of light sensitive semiconductors.

18. Repeating sextant according to claim 17, wherein said light sensitive semiconductors are light sensitive diodes.

19. Repeating sextant according to claim 17, wherein said light sensitive semiconductors are CCDs.

20. Repeating sextant according to claim 13, wherein said sextant is a portable, handheld device which is manually directed toward the celestial body.

21. Repeating sextant according to claim 20, wherein said means for measuring movement about a second axis inhibits said first signal when said second signal exceeds a first predetermined threshold.

22. Repeating sextant according to claim 20, wherein said receiving means is a telescope.

23. Repeating sextant according to claim 22, wherein said detecting means includes an array of light sensitive semiconductors.

24. Repeating sextant according to claim 23, wherein said detecting means inhibits operation of said sextant when an image of the celestial object is not received by said array of light sensitive semiconductors.

25. Repeating sextant according to claim 24, wherein said line of position is determined by comparing said mean altitude with an altitude of the celestial body calculated from said stored ephemerides.

26. A fully automated, repeating sextant comprising:

a lens for receiving a signal from a celestial body;

a first inclinometer for measuring movement of the sextant about a first axis as a first signal which establishes an artificial horizon;

a second inclinometer for measuring roll of the sextant about a second axis, perpendicular to said first axis, as a second signal;

a semiconductor array for detecting the magnitude of at least one signal received from a celestial body and an angle of incidence of the received signal on the semiconductor array, said magnitude and angle of incidence being output by said detecting means;

means responsive to plural values of said first signal and said angle of incidence for determining a mean altitude of the celestial body, and said magnitude being input to said determining means for deriving a calculated altitude of the celestial body from stored data ephemerides, a line of position of the celestial body being determined from said mean altitude and said calculated altitude; and

,

means for displaying the line of position.

27. Repeating sextant according to claim 26, wherein said first and second signals are analog signals which represent an altitude of a centroid of the semiconductor array above a true horizon as determined by the first inclinometer, said sextant further including means for converting said first and second signals to digital signals for input to said altitude and line of position determining means.

28. Repeating sextant according to claim 26, wherein said calculated altitude is determined by applying stored Chebyshev formulae to said stored data ephemerides.

29. An automated, repeating sextant comprising:

an antenna for receiving a signal from a celestial body which emits a radio frequency signal;

a first inclinometer for measuring movement of the sextant about a first axis as a first signal which establishes an artificial horizon;

a second inclinometer for measuring roll of the sextant about a second axis, perpendicular to said first axis, as a second signal;

a radio frequency receiver which identifies the radio frequency signal received by said antenna from said celestial body to determine an azimuth of said celestial body, said azimuth being output by said radio frequency receiver;

means responsive to plural values of said first signal and said azimuth for determining a mean altitude of the celestial body, and determining a line of position using said mean altitude and stored data ephemerides for the celestial body; and

,

means for displaying the line of position.

30. Repeating sextant according to claim 29, wherein a line of position is determined for at least two different celestial bodies to provide a position fix of the sextant, said position fix being displayed on said displaying means.

31. A portable, handheld repeating sextant which is manually directed toward a celestial body comprising:

a telescope for receiving a signal from a celestial body;

a first inclinometer for measuring movement of the sextant about a first axis as a first signal which establishes an artificial horizon;

a second inclinometer for measuring roll of the sextant about a second axis, perpendicular to said first axis, as a second signal, said second inclinometer inhibiting said first signal when said second signal exceeds a first predetermined threshold;

a semiconductor array for detecting the magnitude of at least one signal received from a celestial body and an angle of incidence of the received signal on the semiconductor array, said magnitude and angle of incidence being output by said detecting means;

means responsive to plural values of said first signal and said angle of incidence for determining a mean altitude of the celestial body, and said magnitude being input to said determining means for deriving a calculated altitude of the celestial body from stored data ephemerides, a line of position of the celestial body being determined from said mean altitude and said calculated altitude; and

,

means for displaying the line of position.

32. A repeating sextant according to claim 31, wherein at least one of said first and second signals is an analog signal, said sextant further including means for converting said analog signal to a digital signal for input to said altitude and line of position determining means.

33. Repeating sextant according to claim 32, wherein said mean altitude is statistically enhanced.

34. Repeating sextant according to claim 32, wherein a line of position is determined for at least two different celestial bodies to provide a position fix of the sextant, said position fix being displayed on said displaying means.

35. Repeating sextant according to claim 34, wherein said semiconductor array includes light sensitive semiconductors.

36. A method for determining a line of position from the location of a celestial body comprising the steps of:

receiving a signal from a celestial body;

measuring movement of the sextant about a first axis as a first signal which establishes an artificial horizon;

detecting a signal received from a celestial body using a semiconductor array and an angle of incidence of the received signal on the semiconductor array, said angle of incidence being output by said semiconductor array;

determining plural values of said first signal and said angle of incidence and calculating a mean altitude of the celestial body;

determining a line of position using said mean altitude and stored data ephemerides for the celestial body; and

,

displaying the line of position.

37. Method according to claim 36, wherein a line of position is determined for at least two different celestial bodies to provide a position fix of the sextant, said position fix being displayed.

38. A method for determining a line of position from the location of a celestial body comprising the steps of:

receiving a signal from a celestial body;

measuring movement of the sextant about a first axis as a first signal which establishes an artificial horizon;

detecting a signal received from a celestial body using a radio frequency receiver to determine an azimuth of the celestial body, said azimuth being output by said radio frequency receiver;

determining plural values of said first signal and said azimuth and calculating a mean altitude of the celestial body;

determining a line of position using said mean altitude and stored data ephemerides for the celestial body; and

,

displaying the line of position.