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US3949400A Expired / Lapsed US ⏱️ 0.0 years remaining

Position determination systems

Assignee: National Aeronautics and Space Administration
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Filing: 1973-11-28
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Granted: 1976-04-06
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Expires: 1993-11-28
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Abstract

Abstract Disclosed is a system for an orbital antenna means which is operated at a synchronous altitude to scan an area of a celestial body. The antenna means comprises modules which are operated by a steering signal in a repetitive function for providing a scanning beam over the area. The scanning covers the entire area in a pattern and the azimuth of the scanning beam is transmitted to a control station on the celestial body simultaneous with signals from an activated ground beacon on the celestial body. The azimuth of the control station relative to the antenna means is known and the location of the ground beacon is readily determined from the azimuth determinations.

Inventors

  • 👤 Paul W. Shores

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 20:48
CPC Classifications
G; G01; G01S; G01S5/00; G01S5/02; H; H01; H01Q; H01Q25/00

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 147 words
A method for systematically surveying an area on a celestial body for locating a radio beacon thereon comprising the steps of: a. placing a satellite antenna means, employing a plurality of receive-only scanning beams, in a known synchronous orbit with said celestial body, each of said scanning beams being capable of viewing and receiving radio signals from a unique portion of said area to be surveyed and wherein said scanning beams together completely cover said area to be surveyed; b. continuously and repetitively scanning each of said unique portions of said area to be surveyed with said plurality of scanning beams; c. detecting at the antenna means with one of said scanning beams, the occurrence of radiant wave energy from said radio beacon; and, d. determining the azimuth of said radio beacon with respect to the scanning beam which detected the energy radiated from said radio beacon.
Claim 2
Independent Claim 147 words
A method for systematically surveying an area on a celestial body for locating a radio beacon thereon comprising the steps of: a. placing a satellite antenna means, employing a plurality of receive-only scanning beams, in a known synchronous orbit with said celestial body, each of said scanning beams being capable of viewing and receiving radio signals from a unique portion of said area to be surveyed and wherein said scanning beams together completely cover said area to be surveyed; b. continuously and repetitively scanning each of said unique portions of said area to be surveyed with said plurality of scanning beams; c. detecting at the antenna means with one of said scanning beams, the occurrence of radiant wave energy from said radio beacon; and, d. determining the azimuth of said radio beacon with respect to the scanning beam which detected the energy radiated from said radio beacon.
Claim 3
Dependent Claim 161 words
A remote locating system for determining the position coordinates of a radio beacon emitting radiant energy from an unknown location within an area to be surveyed comprising: a. satellite antenna means, employing a plurality of receive-only scanning beams, and placed in a known synchronous orbit with said celestial body, and wherein each of said scanning beams is capable of viewing and receiving radio signals from a unique portion of said area to be surveyed and wherein said scanning beams together completely cover said area to be surveyed; b. means for continuously and repetitively scanning each of said unique portions of said area to be surveyed with said plurality of scanning beams; c. means for detecting at the antenna means with one of said scanning beams, the occurrence of radiant wave energy from said radio beacon; and, d. means for determining the azimuth of said radio beacon with respect to the scanning beam which detected the energy radiated from said radio beacon.
Claim 4
Dependent Claim 161 words
A remote locating system for determining the position coordinates of a radio beacon emitting radiant energy from an unknown location within an area to be surveyed comprising: a. satellite antenna means, employing a plurality of receive-only scanning beams, and placed in a known synchronous orbit with said celestial body, and wherein each of said scanning beams is capable of viewing and receiving radio signals from a unique portion of said area to be surveyed and wherein said scanning beams together completely cover said area to be surveyed; b. means for continuously and repetitively scanning each of said unique portions of said area to be surveyed with said plurality of scanning beams; c. means for detecting at the antenna means with one of said scanning beams, the occurrence of radiant wave energy from said radio beacon; and, d. means for determining the azimuth of said radio beacon with respect to the scanning beam which detected the energy radiated from said radio beacon.

References Cited (Backward Citations)

US3351942A Cited
US3500411A Cited
US3710255A Cited
US3678387A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-04-06 1979-10-06 1980-04-06 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-04-06 1983-10-06 1984-04-06 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-04-06 1987-10-06 1988-04-06 $7700.00 Window Closed / Lapsed

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