METHOD OF GENERATING CONTROL COMMANDS ON ROCKET ROTATING ON BANKING ANGLE, ROCKET CONTROL SYSTEM, METHOD OF MEASURING BANKING ANGLE ON ROCKET, GYROSCOPIC DEVICE FOR MEASURING BANKING ANGLE, METHOD OF GENERATING SINE AND COSINE SIGNALS ON ROCKET ROTATING ON BANKING ANGLE, AND SINE-COSINE ROCKET CONTROL SYSTEM GENERATOR Russian patent published in 2014 - IPC F42B15/01 

FIELD: physics; control.

SUBSTANCE: group of inventions relates to rocket control systems. The method of generating control commands involves measuring the banking angle of the rocket, which is generated in form of a signal in an n-bit Gray code, which is converted to a binary number having n bits, logic levels of which generate a multi-step approximation of sine-wave and cosine-wave signals, and rocket control commands on the heading and pitch, respectively, are generated from the decoded received signals. The rocket control system includes a gyroscopic device for measuring the banking angle, an XOR logic circuit, a control command converter and a second steering gear. The method of measuring the banking angle involves generating additional sequences of logic levels which form a number in an n-bit Gray code, which is converted to a binary n-bit number which corresponds to the measured value of the banking angle of the rocket. The gyroscopic device for measuring the banking angle further includes LED-photodiode pairs placed on the housing of the gyroscope and separated by raster. The method involves generating sine and cosine signals for generating control commands thereto, wherein a binary number in parallel form is generated in form of an n-bit number. The rocket control system includes a sine-cosine generator of M number setting devices and a digital inverter circuit.

EFFECT: high efficiency of generating control commands for rocket control systems.

8 cl, 6 dwg