method and device for improving the stabilization and maneuverability of unmanned aerial vehicles (uavs) with the use of u0433u0438u0440u043eu0441u043au043eu043fu0438u0447u0435u0441u043au043eu0433u043e effect

摘要

a device (method and device) relates to control systems, is designed to enhance the sustainability and maneuverability, and can be further u044cu0437u043eu0432u0430u043du043e for control and correction of multiple dynamic objects, including small satellites.purpose of the invention is to reduce the sensitivity to the influence of wind and turbulence, without increasing the air speed, but also enhance the sustainability and alone u043eu0432u0440u0435u043cu0435u043du043du043e maneuverability. to improve these parameters, along with the compensation u0433u0438u0440u043eu0441u043au043eu043fu0438u0447u0435u0441u043au043eu0433u043e and reaction points clear, we need to increase the kinetic moment by ki u0440u043eu0441u043au043eu043fu0430.this is achieved in that the gyroscope is installed on the center of gravity of the rotor, with the rotor (opposite the location of the gyroscope is installed in the front of her part, rotation of rotor gyroscope is directed against the rotation of the rotor (the axis of rotation of the gyroscope rotor and rotor are on the same line); the device with you u0441u043eu043au0438u043c u043au0438u043du0435u0442u0438u0447u0435u0441u043au0438u043c momentbecomes less sensitive to the influence of wind and turbulence, increases the stability of flight; to change the flight path of the axis of rotation of the gyroscope rotor rotated by electric motors (motors and gearboxes, stabilization and moments) are located on the axes of rotation of the pivot frames, thusto coincide with the direction of the direction established by the gyroscopic moments turn blah. coincidence of gyroscopic moments with moments of steering wheel height and enhances the maneuverability of uav.stabilization and change of the angular position of the turn around the longitudinal axis, is increased or decreased the speed of rotation of the gyroscope rotor with egr u0443u043bu0438u0440u0443u0435u043cu044bu043c u0438u043du0435u0440u0446u0438u043eu043du043du044bu043c moment.