Patent US3968339A successfully refreshed from Google Patents.
Patent US4049223A successfully refreshed from Google Patents.
US4049223A
Expired / Lapsed
US
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Constant altitude auto pilot circuit
Assignee: United States Department of the Navy
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Filing: 1976-06-21
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Granted: 1977-09-20
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Expires: 1996-06-21
Abstract
Abstract A constant altitude auto pilot circuit samples an altitude electronically d produces error output voltages proportional to the changes in altitude which are used to command the control system of an aircraft. To set the device, the plane obtains the desired altitude whereafter the device is activated. A switch in parallel with an op-amp is closed to charge a capacitor to a voltage level proportional to the output of a transducer. When the switch is opened, all inputs to the op-amp become relative to the charge of the capacitor. Any variation is amplified by the op-amp. Additional inputs allow biasing the altitude signal up or down or introducing a damping signal for control loop stability.
Inventors
- 👤 William S. Watson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 17:49
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/08; G05D1/0808; G05D1/0816
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
198 words
A constant altitude hold auto-pilot which samples an altitude electronically and produces error output voltages proportional to the changes in altitude which are used to command a control system of an aircraft, comprising: an altitude transducer means for providing an analog altitude output signal corresponding to the altitude of an aircraft; a first resistor connected in series with said transducer means; a high impedance input operational amplifier having a positive input, a negative input and an output; a second resistor connected between the output of said first resistor and the output of said operational amplifier; a low leakage capacitor connected between the output of said first resistor and the negative input of said operational amplifier; and, a switch connected between the negative input of said operational amplifier and the output of said operational amplifier, and said switch, when closed, allows said capacitor to charge to a voltage proportionate to the output of said transducer by the operating characteristics of said amplifier, and said switch, when opened on an externally applied altitude hold command signal, allows the capacitor to be in series with the present altitude signal thereby causing the error signal to be amplified by said operational amplifier.
Claim 2
Dependent Claim
198 words
A constant altitude hold auto-pilot which samples an altitude electronically and produces error output voltages proportional to the changes in altitude which are used to command a control system of an aircraft, comprising: an altitude transducer means for providing an analog altitude output signal corresponding to the altitude of an aircraft; a first resistor connected in series with said transducer means; a high impedance input operational amplifier having a positive input, a negative input and an output; a second resistor connected between the output of said first resistor and the output of said operational amplifier; a low leakage capacitor connected between the output of said first resistor and the negative input of said operational amplifier; and, a switch connected between the negative input of said operational amplifier and the output of said operational amplifier, and said switch, when closed, allows said capacitor to charge to a voltage proportionate to the output of said transducer by the operating characteristics of said amplifier, and said switch, when opened on an externally applied altitude hold command signal, allows the capacitor to be in series with the present altitude signal thereby causing the error signal to be amplified by said operational amplifier.
Claim 3
Dependent Claim
25 words
The device of claim 1 including damping and offset signal means connected to the positive input of said operational amplifier for providing control loop stability.
Claim 4
Dependent Claim
39 words
The device of claim 1 including a bias setting means comprising a constant rate ramp signal means which matches the bleed rate of said capacitor, said bias setting means being connected to the positive input of said operational amplifier.
Claim 5
Dependent Claim
39 words
The device of claim 2 including a bias setting means comprising a constant rate ramp signal means which matches the bleed rate of said capacitor, said bias setting means being connected to the positive input of said operational amplifier.
References Cited (Backward Citations)
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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) | 1980-09-19 | 1981-03-21 | 1981-09-20 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-09-19 | 1985-03-21 | 1985-09-20 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-09-19 | 1989-03-21 | 1989-09-20 | $7700.00 | Window Closed / Lapsed |