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US4386355A Expired / Lapsed US ⏱️ 0.0 years remaining

System for determining the location of an airborne vehicle to the earth using a satellite-base signal source

Assignee: Boeing Co
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Filing: 1980-03-31
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Granted: 1983-05-31
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Expires: 2000-03-31
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Abstract

Abstract A satellite in geosynchronous orbit includes a source of signal illumination which is directed toward the earth, covering a given area thereof. An airborne vehicle, such as a missile, traveling over the area covered by the signal illumination from the satellite, includes a first antenna for receiving an incident set of signals from the satellite directly, and a second antenna for receiving the same signals from the satellite after they have been reflected from the earth's surface, referred to as a reflected set of signals. The altitude of the airborne vehicle may be ascertained by comparing the relative times at which the two sets of signals are received at the airborne vehicle, while the remaining location information, referred to as ground map information, may be ascertained by first determining range and angle data from the reflected signals and then comparing that data with ground map data stored aboard the airborne vehicle.

Inventors

  • 👤 Prentis B. Drew
  • 👤 Ervin J. Nalos

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 10:18
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/003; G01S11/00; G01S11/02; G01S5/00; G01S5/02; G01S5/12; G01S7/00; G01S7/003; G01S7/006

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 185 words
A passive system for ascertaining information concerning the position of an airborne vehicle relative to the earth comprising: a signal source located on a base remote from the airborne vehicle; antenna means located on the airborne vehicle for receiving (a) a set of incident signals, said incident signal set comprising signals generated by said signal source and transmitted directly to said antenna means from said signal source, and for receiving (b) a set of reflected signals, said reflected signal set comprising the same signals generated by said signal source but which have been reflected from the earth prior to reaching said antenna means; and means on the airborne vehicle for processing differences in selected characteristics of said incident and reflected sets of signals received by said antenna means, taking into account the angle, if any, between said signal source and the airborne vehicle, including means for comparing the times of receipt of said incident and reflected sets of signals and means for calculating the altitude of the airborne vehicle from the difference in the times of receipt of said incident and reflected sets of signals.
Claim 2
Dependent Claim 185 words
A passive system for ascertaining information concerning the position of an airborne vehicle relative to the earth comprising: a signal source located on a base remote from the airborne vehicle; antenna means located on the airborne vehicle for receiving (a) a set of incident signals, said incident signal set comprising signals generated by said signal source and transmitted directly to said antenna means from said signal source, and for receiving (b) a set of reflected signals, said reflected signal set comprising the same signals generated by said signal source but which have been reflected from the earth prior to reaching said antenna means; and means on the airborne vehicle for processing differences in selected characteristics of said incident and reflected sets of signals received by said antenna means, taking into account the angle, if any, between said signal source and the airborne vehicle, including means for comparing the times of receipt of said incident and reflected sets of signals and means for calculating the altitude of the airborne vehicle from the difference in the times of receipt of said incident and reflected sets of signals.
Claim 3
Dependent Claim 232 words
A passive system for ascertaining information concerning the position of an airborne vehicle relative to the earth, comprising: a signal source located on a base remote from the airborne vehicle; antenna means located on the airborne vehicle for receiving (a) a set of incident signals, said incident signal set comprising signals generated by said signal source and transmitted directly to said antenna means from said signal source, and for receiving (b) a set of reflected signals, said reflected signal set comprising the same signals generated by said signal source but which have been reflected from the earth prior to reaching said antenna means; means on the airborne vehicle for processing differences in selected characteristics of said incident and reflected sets of signals received by said antenna means, taking into account the angle, if any, between said signal source and the airborne vehicle, including means for comparing the times of receipt of said incident and reflected sets of signals and means for comparing the frequencies of said incident and reflected sets of signals; means using the output of said times of receipt comparing means and said frequency comparing means to develop range and azimuth information of the points of reflection on the earth of said reflected set of signals; and map processing means using the range and azimuth information to produce a map of the terrain over which the airborne vehicle is moving.
Claim 4
Dependent Claim 232 words
A passive system for ascertaining information concerning the position of an airborne vehicle relative to the earth, comprising: a signal source located on a base remote from the airborne vehicle; antenna means located on the airborne vehicle for receiving (a) a set of incident signals, said incident signal set comprising signals generated by said signal source and transmitted directly to said antenna means from said signal source, and for receiving (b) a set of reflected signals, said reflected signal set comprising the same signals generated by said signal source but which have been reflected from the earth prior to reaching said antenna means; means on the airborne vehicle for processing differences in selected characteristics of said incident and reflected sets of signals received by said antenna means, taking into account the angle, if any, between said signal source and the airborne vehicle, including means for comparing the times of receipt of said incident and reflected sets of signals and means for comparing the frequencies of said incident and reflected sets of signals; means using the output of said times of receipt comparing means and said frequency comparing means to develop range and azimuth information of the points of reflection on the earth of said reflected set of signals; and map processing means using the range and azimuth information to produce a map of the terrain over which the airborne vehicle is moving.
Claim 5
Dependent Claim 20 words
An apparatus of claim 1 or 2, wherein the base on which said signal source is located is a satellite.
Claim 6
Dependent Claim 14 words
An apparatus of claim 3, wherein said satellite is in a non-inclined, geosynchronous orbit.
Claim 7
Dependent Claim 35 words
An apparatus of claim 1 or 2, wherein said antenna means includes a first, up-looking antenna to receive said set of incident signals, and a second, down-looking antenna to receive said set of reflected signals.
Claim 8
Dependent Claim 26 words
An apparatus of claim 1 or 2, wherein said antenna means includes an omni-directional antenna capable of receiving both said incident and reflected sets of signals.
Claim 9
Dependent Claim 56 words
An apparatus of claim 1 or 2, wherein said processing means includes signal receiving means associated with said antenna means for said incident and reflected sets of signals, pulse detector means associated with each said signal receiver means, and means applying the outputs of the respective pulse detector means to said times of receipt comparing means.

References Cited (Backward Citations)

US2837738A Cited
US3939476A Cited
US3721986A Cited
US3171126A Cited
US3242490A Cited
US3856237A Cited
US3863257A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1986-05-30 1986-11-29 1987-05-31 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1990-05-30 1990-11-29 1991-05-31 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1994-05-30 1994-11-29 1995-05-31 $7700.00 Window Closed / Lapsed

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