FIELD: systems for automatically controlling parameters of interceptor airplane equipment, possible use for controlling its parameters, including limit parameters, in flight.
SUBSTANCE: in accordance to invention, device contains n information sensors, outputs of which are connected to inputs of controllable commutator, comparison block, first input of which is connected to setting block, and output through random-access memory block is connected to first input of indication block, control block, first output of which is connected to control input of controllable commutator, second output - to input of setting block, third output - to second input of indication block, fourth output - to second input of random-access memory block, introduced additionally are serially connected trigger, AND circuits, counter, subtraction circuit, "sine, cosine" transformer, adder and square root computation block, and also supporting phases generator, while the output of square root computation block is connected to second input of comparison block, output of bearing frequency generator - to second input of AND circuit, output of supporting phases generator - to second input of subtraction circuit, and input - to fourth output of control block, while second inputs of trigger and counter are connected to fifth output of control block, and second input of the adder is connected to sixth output of control block.
EFFECT: increased trustworthiness of parameter control in presence of random interference on information sensor outputs.
3 dwg
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|
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Authors
Dates
2007-08-27—Published
1983-05-06—Filed