US4300159A
Expired / Lapsed
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Assignee: National Aeronautics and Space Administration
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Filing: 1975-05-19
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Granted: 1981-11-10
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Expires: 1995-05-19
Abstract
Abstract An aerial vehicle rotating in gyroscopic fashion about one of its axes having an optical system operative to scan an area below the vehicle in determined relation to vehicle rotation. A sensing device is provided to sense the physical condition of the area of scan and optical means are associated therewith to direct the physical intelligence received from the scan area to the sensing means. Means are provided to incrementally move the optical means through a series of steps to effect sequential line scan of the area being viewed keyed to the rotational rate of the vehicle.
Inventors
- 👤 with respect to an invention of Frosch Robert A. Administrator of the National Aeronautics and Space Administration
- 👤 Robert F. Hummer
- 👤 Deane T. Upton
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 18:28
CPC Classifications
H; H04; H04N; H04N7/00; H04N7/002; H04N7/005
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
97 words
In a spin-stabilized satellite positioned in a synchronous orbit whereby the satellite remains in a relatively stationary relationship over an area to be scanned on a terrestrial body, optical means positioned in said satellite and spinning therewith to scan said area, said optical means movable about an axis perpendicular to the spin axis of the satellite, means to induce movement of said optical means in discrete increments keyed to the spin rate of the satellite, and sensing means to receive physical data from the scanned area, said sensing means in an operative arrangement with said optical means.
Claim 2
Dependent Claim
97 words
In a spin-stabilized satellite positioned in a synchronous orbit whereby the satellite remains in a relatively stationary relationship over an area to be scanned on a terrestrial body, optical means positioned in said satellite and spinning therewith to scan said area, said optical means movable about an axis perpendicular to the spin axis of the satellite, means to induce movement of said optical means in discrete increments keyed to the spin rate of the satellite, and sensing means to receive physical data from the scanned area, said sensing means in an operative arrangement with said optical means.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-11-09 | 1985-05-11 | 1985-11-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-11-09 | 1989-05-11 | 1989-11-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-11-09 | 1993-05-11 | 1993-11-10 | $7700.00 | Window Closed / Lapsed |