METHOD FOR FORMING LATERAL-DIRECTIONAL SIGNALS OF NON-STATIONARY UNMANNED AERIAL VEHICLE WITH ADAPTIVE-FUNCTIONAL CORRECTION AND A DEVICE FOR ITS IMPLEMENTATION Russian patent published in 2017 - IPC G05D1/00 B64C13/02 

FIELD: aviation.

SUBSTANCE: to form a control signal, an angle of yaw is set, the yaw angle signal is measured, a course error signal is formed, a roll control signal is limited, angular velocity signals of roll, heading and ram air are measured, the signal of the heading error and heading angular velocity are amplified, the received signals are summed up, the correcting amplification of the heading error signal is inverted, scaling of the sum signal is inverted, the setpoint of the coordinating roll control signal is formed, a roll correcting component is formed, a basic roll control signal is formed in a certain manner, an output control signal, limited in a certain manner, is formed. The device contains a heading angle selector, two computing units, a heading angle sensor, two signal limiters, a roll angle sensor, a heading angular velocity sensor, a roll angular velocity sensor, a ram air sensor, two adaptive summing amplifiers, an adaptive-corrective inverting amplifier, an adaptive signal limiter, an adaptive inverting scaling amplifier, interconnected in a certain way.

EFFECT: expansion of functional capabilities for flight in a wide range of trajectories.

2 cl, 1 dwg