Patent US4176353A successfully refreshed from Google Patents.
US4176353A
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Radar altimeter tracking circuit apparatus
Assignee: Honeywell Inc
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Filing: 1978-02-24
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Granted: 1979-11-27
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Expires: 1998-02-24
Abstract
Abstract A radar altimeter having a tracking circuit which includes a controllable reference signal generator which is adapted to selectively control the tracking circuit so that there will be no indication of an altitude change in the event of a momentary loss of a received video signal due to the fading of the video signal or other condition requiring the locking of the tracking circuit because of a lack of reliability of the received video signal.
Inventors
- 👤 Robert P. Pearson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 11:54
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/02; G01S13/06; G01S13/08; G01S13/10; G01S13/18
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
238 words
A radar altimeter for determining the altitude of a craft above a surface comprising: a radar pulse transmitter adapted to transmit radio frequency pulses; a receiver adapted to receive reflected radio frequency pulses from a surface, said receiver including means to produce video signals having an amplitude corresponding to the reflected pulses; a gate pulse generator connected to said transmitter to produce a gate signal pulse following each transmitted pulse and displaced in time from each of said transmitted pulses by an amount corresponding to a prior altitude signal determined by the transit time of a transmitted pulse to radiate to the surface and back to said receiver during a previous transmission; pulse signal comparison means connected to said receiver and to said gate pulse generator to produce on the output thereof a control signal having an amplitude indicative of any signal overlap between a video signal from said receiver and said gate signal pulse; a reference signal pulse generating source having an output connected to an output of said pulse signal comparison means and having an output signal pulse thereon whose amplitude represents a predetermined standard for comparison with said control signal on the output of said pulse signal comparison means; and means connecting the video signals from said receiver to an input of said reference signal pulse generating source to activate said reference signal source only upon the occurrence of a video signal from said receiver.
Claim 2
Dependent Claim
238 words
A radar altimeter for determining the altitude of a craft above a surface comprising: a radar pulse transmitter adapted to transmit radio frequency pulses; a receiver adapted to receive reflected radio frequency pulses from a surface, said receiver including means to produce video signals having an amplitude corresponding to the reflected pulses; a gate pulse generator connected to said transmitter to produce a gate signal pulse following each transmitted pulse and displaced in time from each of said transmitted pulses by an amount corresponding to a prior altitude signal determined by the transit time of a transmitted pulse to radiate to the surface and back to said receiver during a previous transmission; pulse signal comparison means connected to said receiver and to said gate pulse generator to produce on the output thereof a control signal having an amplitude indicative of any signal overlap between a video signal from said receiver and said gate signal pulse; a reference signal pulse generating source having an output connected to an output of said pulse signal comparison means and having an output signal pulse thereon whose amplitude represents a predetermined standard for comparison with said control signal on the output of said pulse signal comparison means; and means connecting the video signals from said receiver to an input of said reference signal pulse generating source to activate said reference signal source only upon the occurrence of a video signal from said receiver.
Claim 3
Dependent Claim
53 words
An altimeter as claimed in claim 1 wherein said reference signal source has input means connected to outputs of said receiver and said gate pulse generator so that said source will be activated upon the occurrence of a video signal from said receiver and said gate signal pulse from said gate pulse generator.
Claim 4
Dependent Claim
28 words
An altimeter as claimed in claim 2 wherein said reference signal pulse generating source comprises a monostable multivibrator having an output pulse whose amplitude represents said predetermined standard.
Claim 5
Dependent Claim
199 words
A radar altimeter for determining the altitude of a craft above a surface which altimeter includes a signal transmitter, a signal receiver which is adapted to produce a return signal following a signal transmission by the signal transmitter and a closed loop tracking circuit, the improvement comprising: a gate pulse generator connected in said tracking circuit to form a part thereof and to an output of said transmitter to produce a gate signal pulse positioned in time to represent a previous altitude determination; pulse signal comparison means connected in said tracking circuit to form a further part thereof and to receive on inputs thereof a return signal from said signal receiver and a signal from said gate pulse generator to produce a control signal having an amplitude indicative of any signal overlap between said return signal and said gate signal pulse; a reference pulse generating source connected to said pulse signal comparison means and having an output signal whose amplitude represents a predetermined standard for comparison with said control signal from said pulse signal comparison means; and reference signal control means connected to activate said signal reference pulse generating source only upon the occurrence of an input control signal.
Claim 6
Dependent Claim
199 words
A radar altimeter for determining the altitude of a craft above a surface which altimeter includes a signal transmitter, a signal receiver which is adapted to produce a return signal following a signal transmission by the signal transmitter and a closed loop tracking circuit, the improvement comprising: a gate pulse generator connected in said tracking circuit to form a part thereof and to an output of said transmitter to produce a gate signal pulse positioned in time to represent a previous altitude determination; pulse signal comparison means connected in said tracking circuit to form a further part thereof and to receive on inputs thereof a return signal from said signal receiver and a signal from said gate pulse generator to produce a control signal having an amplitude indicative of any signal overlap between said return signal and said gate signal pulse; a reference pulse generating source connected to said pulse signal comparison means and having an output signal whose amplitude represents a predetermined standard for comparison with said control signal from said pulse signal comparison means; and reference signal control means connected to activate said signal reference pulse generating source only upon the occurrence of an input control signal.
Claim 7
Dependent Claim
32 words
An altimeter as claimed in claim 4 wherein said reference signal control means connected to said receiver will activate said reference signal source only upon the occurrence of a proper return signal.
Claim 8
Dependent Claim
66 words
An altimeter as claimed in claim 5 wherein said reference signal control means is connected to an input means of said reference signal source and to outputs of said signal receiver and said gate pulse generator so that upon the occurrence of a return signal from said signal receiver and said gate signal pulse from said gate pulse generator said reference signal source will be activated.
Claim 9
Dependent Claim
28 words
An altimeter as claimed in claim 6 wherein said signal reference pulse generating source comprises a monostable multivibrator having an output pulse whose amplitude represents said predetermined standard.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-11-26 | 1983-05-28 | 1983-11-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-11-26 | 1987-05-28 | 1987-11-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-11-26 | 1991-05-28 | 1991-11-27 | $7700.00 | Window Closed / Lapsed |