← Back to Patent Explorer
US3371161A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of electronic stabilization of the image obtained with a television camera rigidly installed on a moving support

Assignee: Nord Aviation Societe Nationale de Constructions Aeronautiques
•
Filing: 1964-03-23
•
Granted: 1968-02-27
•
Expires: 1984-03-23
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

No abstract record available.

Inventors

  • 👤 Crovella Christian-Charles

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 03:12
CPC Classifications
G; G02; G02B; G02B27/00; G02B27/64; G02B27/644; F; F41; F41G; F41G7/00; F41G7/20; F41G7/22; F41G7/2253; F41G7/2273; F41G7/2293

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 238 words
APPARATUS FOR COMPENSATING FOR MOVEMENTS OF THE OPTICAL IMAGE PRODUCED IN THE TUBE OF A TELEVISION CAMERA MOUNTED ABOARD AN AIRCRAFT AND PLACED ON A SUPPORT RIGIDLY SECURED TO SAID AIRCRAFT, WHICH MOVEMENTS OF THE OPTICAL IMAGE RESULT FROM RELATIVE MOVEMENTS BETWEEN THE CAMERA ON ITS SUPPORT AND AN OBJECT TO BE FILMED DUE TO MOVEMENT OF THE AIRCRAFT ABOUT ITS PITCHING, ROLLING AND YAWING AXES COMPRISING GYROSCOPIS MEANS FOR DETECTING AND MEASURING THE ANGLES OF YAWING, PITCHING, AND ROLLING OF THE AIRCRAFT, A TELEVISION CAMERA RIGIDLY MOUNTED ON A SUPPORT SECURED TO THE AIRCRAFT FOR MOVEMENT THEREWITH, SAID TELEVISION CAMERA HAVING A TUBE WITH ELECTRON GUN MEANS TO PRODUCE AN ELECTRON BEAM AND DEFLECTING COIL MEANS ASSOCIATED THEREWITH, MEANS CONNECTED TO SAID GYROSCOPIC MEANS FOR FORMING AND APPLYING DEVIATION VOLTAGES, SAID MEANS SUPPLYING ELECTRICAL SIGNALS WHICH ARE A FUNCTION OF MOVEMENT OF SAID GYROSCOPIC MEANS TO SAID DEFLECTING COIL MEANS OF SAID TELEVISION CAMERA TUBE, SAID GYROSCOPIC MEANS INCLUDING AT LEAST ONE DIRECTIONAL GYROSCOPE HAVING PRIMARY AND SECONDARY RINGS AND FREELY MOUNTED ON SAID SUPPORT SECURED TO THE AIRCRAFT WITH AXES CONNECTED TO SAID PRIMARY AND SECONDARY RINGS RESPECTIVELY TO DRIVE SAID MEANS FOR FORMING AND APPLYING DEVIATION VOLTAGES INCLUDING DETECTING MEANS FOR DETECTING THE ANGLES OF PITCHING AND YAWNING RESPECTIVELY, THE OUTPUT VOLTAGES OF SAID DETECTING MEANS BRING SIMULTANEOUSLY APPLIED WITH CORRESPONDING VOLTAGES AT IMAGE FREQUENCY AND LINE SCANNING FREQUENCY, RESPECTIVELY, TO SAID DEFLECTING COIL MEANS,
Claim 2
Dependent Claim 238 words
APPARATUS FOR COMPENSATING FOR MOVEMENTS OF THE OPTICAL IMAGE PRODUCED IN THE TUBE OF A TELEVISION CAMERA MOUNTED ABOARD AN AIRCRAFT AND PLACED ON A SUPPORT RIGIDLY SECURED TO SAID AIRCRAFT, WHICH MOVEMENTS OF THE OPTICAL IMAGE RESULT FROM RELATIVE MOVEMENTS BETWEEN THE CAMERA ON ITS SUPPORT AND AN OBJECT TO BE FILMED DUE TO MOVEMENT OF THE AIRCRAFT ABOUT ITS PITCHING, ROLLING AND YAWING AXES COMPRISING GYROSCOPIS MEANS FOR DETECTING AND MEASURING THE ANGLES OF YAWING, PITCHING, AND ROLLING OF THE AIRCRAFT, A TELEVISION CAMERA RIGIDLY MOUNTED ON A SUPPORT SECURED TO THE AIRCRAFT FOR MOVEMENT THEREWITH, SAID TELEVISION CAMERA HAVING A TUBE WITH ELECTRON GUN MEANS TO PRODUCE AN ELECTRON BEAM AND DEFLECTING COIL MEANS ASSOCIATED THEREWITH, MEANS CONNECTED TO SAID GYROSCOPIC MEANS FOR FORMING AND APPLYING DEVIATION VOLTAGES, SAID MEANS SUPPLYING ELECTRICAL SIGNALS WHICH ARE A FUNCTION OF MOVEMENT OF SAID GYROSCOPIC MEANS TO SAID DEFLECTING COIL MEANS OF SAID TELEVISION CAMERA TUBE, SAID GYROSCOPIC MEANS INCLUDING AT LEAST ONE DIRECTIONAL GYROSCOPE HAVING PRIMARY AND SECONDARY RINGS AND FREELY MOUNTED ON SAID SUPPORT SECURED TO THE AIRCRAFT WITH AXES CONNECTED TO SAID PRIMARY AND SECONDARY RINGS RESPECTIVELY TO DRIVE SAID MEANS FOR FORMING AND APPLYING DEVIATION VOLTAGES INCLUDING DETECTING MEANS FOR DETECTING THE ANGLES OF PITCHING AND YAWNING RESPECTIVELY, THE OUTPUT VOLTAGES OF SAID DETECTING MEANS BRING SIMULTANEOUSLY APPLIED WITH CORRESPONDING VOLTAGES AT IMAGE FREQUENCY AND LINE SCANNING FREQUENCY, RESPECTIVELY, TO SAID DEFLECTING COIL MEANS,

References Cited (Backward Citations)

US2869803A Cited
US3240942A Cited
US3240860A Cited
US3293360A Cited
US3261912A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1971-02-26 1971-08-28 1972-02-27 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1975-02-26 1975-08-28 1976-02-27 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1979-02-26 1979-08-28 1980-02-27 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag