Constant altitude auto pilot circuit
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorWilliam S. Watson
Life of this patent
Estimating the term…
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.
Claims4
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.
Dependencies are inferred from the claim text.