초록

A device for counting oscillations of an oscillating temporal signal. The device comprises means for counting all the alternate crossings of a positive threshold value and of a negative threshold value by a monitored time signal.

대표청구항 ▼

1. A device for counting oscillations of an oscillating time signal, which comprises: a first comparator which receives said time signal and which compares it to a first threshold value which is positive;a first AND logic gate, a first input of which is linked to the output of said first comparator;

1. A device for counting oscillations of an oscillating time signal, which comprises: a first comparator which receives said time signal and which compares it to a first threshold value which is positive;a first AND logic gate, a first input of which is linked to the output of said first comparator;a first two-input bistable flip-flop, a signal input of which is linked to the output of said first AND logic gate;a first inverter which is mounted between the output of said first bistable flip-flop and the second input of said first AND logic gate;a second comparator which also receives said time signal and which compares it to a second threshold value which is negative, the output of said second comparator being linked to an initialization input of said first bistable flip-flop;a second AND logic gate, a first input of which is linked to the output of said second comparator;a second two-input bistable flip-flop, a signal input of which is linked to the output of said second AND logic gate, and an initialization input of which is linked to the output of said first comparator;a second inverter which is mounted between the output of said second bistable flip-flop and the second input of said second AND logic gate;an OR logic gate, the two inputs of which are linked respectively to the outputs of said first and second AND logic gates, and the output of which controls a switching means to generate a unit value intended to increment a counter, each time said time signal exceeds, alternatively, one of said first and second threshold values; andsaid counter which is thus incremented and which handles the counting of the oscillations of said oscillating time signal. 2. The device as claimed in claim 1, which comprises, in addition, a delay unit which stores a unit value at the output of the OR logic gate for a predetermined duration before sending it to an auxiliary means mounted at the output of said counter to decrement the latter as appropriate. 3. The device as claimed in claim 1, which comprises, in addition, at least one bandpass filtering means for filtering the time signal before transmitting it to said first and second comparators. 4. The device as claimed in claim 1, which comprises, in addition, a high-pass filtering means for filtering the time signal before transmitting it to said first and second comparators. 5. The device as claimed in claim 1, which comprises, in addition, a comparison means for comparing the value obtained from said counter with a predetermined value and for sending an output signal immediately said value obtained from said counter, which represents the number of half-periods of oscillations counted, becomes greater than said predetermined value. 6. The device as claimed in claim 1, which comprises, in addition: means for previously breaking down the oscillating time signal into a plurality of frequency bands; andmeans for performing a separate count in each duly formed frequency band. 7. The device as claimed in claim 1, wherein said first and second threshold values present the same absolute value. 8. A device for automatically detecting at least one oscillatory failure in at least one position-mode servo-control subsystem of at least one control surface of an aircraft, said subsystem forming part of an electrical flight control system of the aircraft and comprising: said control surface which is mobile, and the position of which relative to the aircraft is set by at least one actuator;said actuator which sets the position of said control surface, according to at least one received actuation order;at least one sensor which measures the actual position of said control surface; anda computer which generates a control surface control order, which receives said measured actual position and which deduces therefrom an actuation order which is transmitted to said actuator,said device comprising: first means for estimating, using said control surface control order, a theoretical position corresponding to a reference position of said control surface in the absence of failure;second means for calculating the difference between said theoretical position estimated by said first means and the actual position measured by said sensor so as to form a residual value; andthird means for: comparing this residual value to at least one predetermined threshold value;performing a count of all the successive and alternate overshoots of said predetermined threshold value by said residual value; anddetecting an oscillatory failure immediately the number resulting from said count becomes greater than a predetermined number,wherein said third means comprise an oscillation counting device, as specified under claim 1. 9. An electrical flight control system of an aircraft, said system comprising at least one means for generating a control surface control order for at least one control surface of the aircraft and at least one position-mode servo-control subsystem of this control surface, which comprises: said control surface which is mobile, and the position of which relative to the aircraft is set by at least one actuator;said actuator which sets the position of said control surface, according to at least one received actuation order;at least one sensor which measures the actual position of said control surface; anda computer which generates said control surface control order, which receives said actual position and which deduces therefrom an actuation order which is transmitted to said actuator, which comprises, in addition, at least one device for automatically detecting at least one oscillatory failure in said servo-control subsystem, as specified under claim 8.