| 摘要 |
FIELD: aircraft control systems. SUBSTANCE: proposed system includes aircraft position selectors showing change of aircraft position relative to axes of body-axis coordinate system, sensors of angular rate relative to coordinate system, angle- of-attack and side-slip sensors, flight altitude sensors, ram air pressure sensors and g-load sensor, undercarriage leg position and compression sensors, drives of aerodynamic aircraft position control members relative to axes of coordinate system, devices changing direction of engine thrust vector and drive control unit which is connected to selectors and sensors including computers of pitch, heading and roll control channels, adders of signals of computers of pitch, roll and heading control channels, control signal correctors of units changing direction of thrust vector which may be provided with devices for forming computers, correctors and adders or may be made for performing functions corresponding to combinations of computers, correctors and adders. EFFECT: possibility of controlling aircraft at super-low flying speeds, performing maneuvers at high angles of attack at increased rate of change of position. 5 cl, 1 dwg
|
