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Novel azimuthal control system flexible to operate

A direction control and flexible technology, applied in entertainment, toys, toy airplanes, etc., can solve the problems of large size, tail servo offset, and inability to maintain position

Inactive Publication Date: 2016-07-20
李宜汉
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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

Method used

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  • Novel azimuthal control system flexible to operate
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Embodiment Construction

[0016] The new flexible azimuth control system shown in the present invention adopts the steering angle vector control device, which is specially designed for the mold lifting machine, and combines the sensor and the controller together. Since the function of the new flexible azimuth control system is to adjust The steering gear, mainly the offset of the tail steering gear, assists in adjusting the steering of the molded aircraft to make its flight control more precise.

[0017] Such as figure 1 with figure 2 As shown, the novel azimuth control system with flexible manipulation is composed of a skeleton with a control panel 100 and an integrated circuit board (not shown) built in it. The function keys on the control panel 100 correspond to the corresponding function keys on the integrated circuit board. The module is electrically connected, and the integrated circuit board is electrically connected to the tail steering gear and the receiving device, wherein the receiving dev...

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Abstract

The invention provides a novel azimuthal control system flexible to operate. The azimuthal control system is composed of a skeleton which is provided with an operating panel and an integrated circuit board which is arranged in the skeleton, wherein a working mode display and a plurality of mode switching buttons are arranged on the panel. According to the novel azimuthal control system flexible to operate, a sensor and a control are integrally combined, and the debugging mode of a steering engine is selected by virtue of a working condition regulating knob; and the azimuthal control system disclosed by the invention is small and thin in size and relatively light in weight, and flight energy consumption can be effectively reduced, so that time of endurance 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...

Claims

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Application Information

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IPC IPC(8): A63H27/20A63H29/22
Inventor 李宜汉
Owner 李宜汉
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