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US3624366A Expired / Lapsed US ⏱️ 0.0 years remaining

Vertical flight path error altimeter

Assignee: Kollsman Instrument Corp
•
Filing: 1969-01-29
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Granted: 1971-11-30
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Expires: 1989-01-29
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Abstract

Abstract A vertical flight path error indicating system is disclosed for presenting an easily interpretable indication of vertical flight path error to show the direction and degree of the error and the rate of correction of the error. In the illustrative disclosure a typical approach and landing sequence is described and equipment is shown for computing the horizontal distance covered, the required corresponding altitude, and the true altitude. A signal is generated to represent the difference between required and true altitude and a movable index is positioned relative to an altitude deviation scale under the control of the signal.

Inventors

  • 👤 James W Angus

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 19:24
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/04; G05D1/06; G05D1/0607; G05D1/0653; G05D1/0676; G01; G01C; G01C23/00; G01S; G01S1/00; G01S1/02

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 209 words
In a vertical flight path control system for an aircraft that includes actual flight data input means for providing a first signal representative of horizontal distance traveled by the aircraft and a second input signal representative of actual altitude of the aircraft, apparatus for programming a desired vertical flight path and for comparing actual altitude with programmed altitude corresponding to the horizontal position of the aircraft along the desired flight path, said apparatus comprising first means settable in accordance with the horizontal distance to be traveled by the aircraft along the desired flight path and responsive to said first input signal to provide a horizontal distance reference signal representative of the instantaneous proportion of the horizontal distance of the desired flight path traveled by the aircraft, second means settable in accordance with the altitude at which the aircraft is to fly at predetermined locations along the desired flight path and responsive to said horizontal reference signal to produce an altitude reference signal representative of programmed altitude corresponding to the instantaneous horizontal location of the aircraft along the desired flight path, and third means responsive to said second input signal and said altitude reference signal for producing an error signal representative of the deviation between actual altitude and programmed altitude.
Claim 2
Dependent Claim 209 words
In a vertical flight path control system for an aircraft that includes actual flight data input means for providing a first signal representative of horizontal distance traveled by the aircraft and a second input signal representative of actual altitude of the aircraft, apparatus for programming a desired vertical flight path and for comparing actual altitude with programmed altitude corresponding to the horizontal position of the aircraft along the desired flight path, said apparatus comprising first means settable in accordance with the horizontal distance to be traveled by the aircraft along the desired flight path and responsive to said first input signal to provide a horizontal distance reference signal representative of the instantaneous proportion of the horizontal distance of the desired flight path traveled by the aircraft, second means settable in accordance with the altitude at which the aircraft is to fly at predetermined locations along the desired flight path and responsive to said horizontal reference signal to produce an altitude reference signal representative of programmed altitude corresponding to the instantaneous horizontal location of the aircraft along the desired flight path, and third means responsive to said second input signal and said altitude reference signal for producing an error signal representative of the deviation between actual altitude and programmed altitude.
Claim 3
Dependent Claim 41 words
In a vertical flight path control system in accordance with claim 1 wherein said first means includes means controlled by said first input signal and responsive to a preset horizontal distance difference signal for presenting said horizontal reference signal as output.
Claim 4
Dependent Claim 70 words
In a vertical flight path control system in accordance with claim 1 wherein said first means includes means controlled by said first input signal and responsive to a preset horizontal distance difference signal for presenting said horizontal reference signal as output, and wherein said second means includes means controlled by said horizontal reference signal and responsive to a preset altitude difference signal for presenting said altitude reference signal as output.
Claim 5
Dependent Claim 157 words
In a vertical flight path control system in accordance with claim 1 wherein said first means includes a distance potentiometer having a movable wiper, means including a pair of potentiometers connected to determine a seleCted voltage range across said distance potentiometer representative of the horizontal distance of the desired flight path, and control means responsive to said first input signal for moving said wiper in accordance with the proportion of the horizontal distance of the desired flight path traveled by the aircraft, and wherein said second means includes an altitude potentiometer having a movable wiper, means including a pair of potentiometers connected to determine a selected voltage range across said altitude potentiometer representative of altitude variation of the desired flight path, said control means including mechanical means for moving the wiper of said altitude potentiometer in ganged relation with the wiper of said distance potentiometer whereby said horizontal reference signal is in the form of mechanical position.

References Cited (Backward Citations)

US3081969A Cited
US2987275A Cited
US3157877A Cited
US3266040A Cited
US3279724A Cited
US3309707A Cited
FR1517949A Cited
FR92519E Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-11-29 1975-05-31 1975-11-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-11-29 1979-05-31 1979-11-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-11-29 1983-05-31 1983-11-30 $7700.00 Window Closed / Lapsed

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