Arrangement for controlling the position of an aircraft control surface
First Claim
1. An arrangement for controlling the position of an aircraft control surface member, comprising:
- means for supplying electric power;
means for issuing an electric input signal having a value that is indicative of the desired position of the control surface member at least while electric power is being supplied by said supplying means;
means for amplifying said input signal, including an input terminal receiving said input signal and an output terminal carrying an output signal;
means connected to said output terminal and operative for positioning the control surface member in dependence on said output signal;
means for storing electric charge, including one terminal connected to said input terminal of said amplifying means and another terminal connected to said output terminal, said storing means being discharged upon interruption of the supply of electric power by said supplying means and recharged with a predetermined time constant upon restoration of such supply;
means for detecting the restoration of the supply of electric power by said supplying means and issuing a switching signal for a predetermined time interval immediately following such restoration; and
means for recharging said storing means to said correct value immediately after the restoration with a time constant amounting at most to a small fraction of said predetermined time constant, including means for grounding said one terminal of said storing means in response to and for the duration of said switching signal.
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Accused Products
Abstract
An arrangement for controlling the position of a movable member, especially an aircraft control surface member, includes an operational amplifier and a capacitor connected in parallel to the amplifier. The control arrangement further includes a detector which detects the restoration of the supply of electric power following its interruption and generates a limited-duration pulse. This pulse is then used to close a switch, which is interposed between an input terminal of the capacitor and the ground, for the duration of this pulse, so that the capacitor is charged much more rapidly than otherwise. The output signal of the combination of the operational amplifier and the capacitor is supplied to an actuator for the movable member so that the extent of excursion of the movable member out of its desired position after the electric power supply has been restored is minimized.
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Citations
14 Claims
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1. An arrangement for controlling the position of an aircraft control surface member, comprising:
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means for supplying electric power; means for issuing an electric input signal having a value that is indicative of the desired position of the control surface member at least while electric power is being supplied by said supplying means; means for amplifying said input signal, including an input terminal receiving said input signal and an output terminal carrying an output signal; means connected to said output terminal and operative for positioning the control surface member in dependence on said output signal; means for storing electric charge, including one terminal connected to said input terminal of said amplifying means and another terminal connected to said output terminal, said storing means being discharged upon interruption of the supply of electric power by said supplying means and recharged with a predetermined time constant upon restoration of such supply; means for detecting the restoration of the supply of electric power by said supplying means and issuing a switching signal for a predetermined time interval immediately following such restoration; and means for recharging said storing means to said correct value immediately after the restoration with a time constant amounting at most to a small fraction of said predetermined time constant, including means for grounding said one terminal of said storing means in response to and for the duration of said switching signal. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. An arrangement for controlling an actuator that adjusts the position of a movable member in dependence on the value of an electric control signal when electric power is being supplied thereto from a source, comprising
means for amplifying the control signal, including an input terminal receiving the control signal and an output terminal carrying an output signal; -
means connected to said output of said amplifying means at a juncture and operative for conducting an output signal received from said output terminal to the actuator; means for storing electric charge, including one terminal connected to said input terminal of said amplifying means and another terminal connected to said output terminal, said storing means being discharged upon interruption of the supply of electric power by the source and recharged with a predetermined time constant upon restoration of such supply; means for detecting the restoration of the supply of electric power by the source and issuing a switching signal for a predetermined time interval immediately following such restoration; and means for recharging said storing means to said correct value immediately after the restoration with a time constant amounting at most to a small fraction of the predetermined time constant, including means for grounding said one terminal of said storing means in response to and for the duration of said switching signal. - View Dependent Claims (9, 10, 11, 12, 13, 14)
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Specification