METHOD FOR GENERATION OF COMMAND INDEX OF AIRCRAFT THRUST CONTROL AND DEVICE TO THIS END Russian patent published in 2014 - IPC B64D45/00 

FIELD: aircraft engineering.

SUBSTANCE: proposed method comprises the measurement of aircraft current coordinate and flight parameters, loading said parameters to computer, defining full power reference magnitude and specific full power, defining current full power and specific full power, comparing reference power with current specific power, definition and visualisation of error in control over full power by generation of moving director demand on display of flight command instrument. Director demand generator for control aircraft thrust comprises unit 1 of communication with onboard measuring hardware, unit 2 to compute flight basis coordinates V and h, unit 3 to compute reference flight full power, unit 4 to compute reference magnitude of power height, unit 5 to compute flight current full power, unit 6 to compute current magnitude of power height, and unit 7 to compute error in control over power height. Output signal of unit 7 is transmitted to director to display in the field of vision of pilot an extra director demand for control over engine thrust.

EFFECT: higher accuracy of control and flight safety.

2 cl, 4 dwg