ADAPTIVE SYSTEM FOR CONTROLLING FLIGHT HEIGHT OF AN AIRCRAFT Russian patent published in 2006 - IPC G05D1/04 

FIELD: engineering of onboard systems for automatic control of aircrafts, which during flight realize turns at significant angles of attack.

SUBSTANCE: control system contains aircraft as control object, steering drive, device for measuring angular position by pitch, adding amplifier, speed force indicator, indicator of height and height alternation speed, flight speed indicator, height signal set-point device, discrepancy block, first signal limiting block, functional transformer, second signal limiting block, functional device for limiting signal, first set-point device of bearing signal, first division block and first multiplication block, while functional transformer contains two of each of the following: set-point device of bearing signal, division block, multiplication block and adder.

EFFECT: expanded functional capabilities, limitation of angle of attack of an aircraft.

2 cl, 3 dwg