Novel flexible-to-operate azimuth control system

Abstract

The invention provides a novel flexible-to-operate azimuth control system, which consists of a framework and an integrated circuit board, wherein the framework is provided with an operation and control panel; the integrated circuit board is built in the framework; and a work mode display and a plurality of mode switching press buttons are arranged on the panel. A sensor and a controller of the novel flexible-to-operate azimuth control system are combined into a whole; and the debugging mode of a steering engine can be selected through a work state regulating knob. The novel flexible-to-operate azimuth control system has the advantages that the size is small; the weight is light; the flight energy consumption can be effectively reduced; and the endurance time is prolonged.

Description

technical field [0001] The invention relates to a model airplane product, in particular to a novel and flexible azimuth control system on a model helicopter. Background technique [0002] When the model helicopter is hovering in the air, sometimes it will be hit by the side wind. At this time, the tail servo of the helicopter will deviate in the horizontal direction. In order to correct this deviation, the tail servo installed on the helicopter The azimuth control system will send a control signal to the tail servo to resist the deviation of the tail servo in the opposite direction. When the tail steering gear stops drifting, the control signal of the azimuth control system also disappears thereupon. If the crosswind continuously hits the helicopter, it will cause the tail servo to continuously shift. At this time, the azimuth control system will always resist the deviation of the tail servo until the tail servo moves to the leeward position. This is the weather vane effect...

AI Technical Summary

Problems solved by technology

If the crosswind continuously hits the helicopter, it will cause the tail servo to continuously shift. At this time, the azimuth control system will always resist the deviation of the tail servo until the tail servo moves to the leeward position. This is the weather vane effect. As a result, the tail steering gear is offset, and the original position cannot be maintained; secondly, the traditional azimuth control system only sends a control signal to the tail steering gear when the tail steering gear of the helicopter moves, and when the tail steering gear stops When moving, the control signal also returns to zero, which causes the azimuth control system to be unable to control the tail steering gear in time; in addition, the traditional azimuth control system is large in size and heavy in weight, which consumes the energy of the helicopter during flight, thereby reducing Helicopter flight time

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