| 摘要 |
FIELD: aviation pilotage with processor control sets. ^ SUBSTANCE: control system is used for limiting the angle of attack and normal g-load, limiting the deviation of rudder, control of deflectable wing leading-edges, control of flaps and re-programming aircraft stability and controllability characteristics. Four-channel computer parts of system is used for conveyer processing of information. Each channel of computer parts os used for determination of control signals in "channel-model" structure by converting the signals of sensors; sensors are controlled by means of information input receivers; in the course of determination, use is made of solving and model processors; analog-to-digital converters and single command registers are used for control of drivers at closing the inner circuits of one channel of all drivers, amplifying the commands in current and voltage; system is used for transmission of feedback signals to digital computer, monitoring the computer parts, feeding the electrical units and sensors with stabilized voltage, closing the external circuit through digital computer part and closing the internal circuit through analog computer part. ^ EFFECT: enhanced efficiency of aircraft control; extended functional capabilities. ^ 8 cl, 4 dwg |
