Aviation flight system with strong shake resistance
An anti-seismic performance and aeronautical technology, applied in the field of molded aircraft, can solve the problems of reduced vibration-absorbing ability, poor neutral point characteristics, and setting, and achieve the effect of improving anti-seismic performance and small size
Inactive Publication Date: 2016-07-27
马铿杰
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Problems solved by technology
The operator of the toy aircraft cannot set various parameters for controlling the flight of the toy aircraft on the azimuth indicator of the toy aircraft without an operation panel
In addition, all the induction devices of the aviation flight system with strong anti-seismic performance are also relatively large in size, which leads to the reduction of the vibration-absorbing ability of the aviation flight system with strong anti-seismic performance, and also makes the neutral point characteristics worse
Method used
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Embodiment Construction
[0011] Embodiments of the present invention will now be described in conjunction with the accompanying drawings.
[0012] see figure 1 , the aviation flight system with strong anti-seismic performance of the present invention is used for toy aircraft, and is connected with the receiving device and the tail rudder servo on the toy aircraft, including remote control device 22 and induction equipment 33 connected with remote control device 22, remote control device 22 An operation panel 23 is arranged on the top, and a liquid crystal display 231 is arranged on the operation panel 23 , and a plurality of buttons 232 and 233 are also arranged below the liquid crystal display 231 on the operation panel 23 . In combination with the plurality of buttons 232 and 233 and the LCD display 231, the operator of the toy aircraft can precisely set the parameters required to control the flight of the toy aircraft.
[0013] The sensing device 33 has a maximum diameter of not more than 30 mm an...
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The invention discloses an aviation flight system with strong shake resistance. The aviation flight system comprises a remote control device and a sensing device connected with the remote control device, wherein an operation panel is arranged on the remote control device, a liquid crystal display screen is arranged on the operation panel, and a plurality of buttons are further arranged below the liquid crystal display screen on the operation panel. According to the aviation flight system, the plurality of buttons are used for setting and changing various parameters needed for controlling a toy aircraft at any time, the parameter variation is displayed through the liquid crystal display screen in real time, and thus an operator can set the needed parameters accurately. In addition, the adopted sensing device is small in size, and therefore, the shake resistance of the aviation flight system is improved.
Description
technical field [0001] The invention relates to a mold aircraft, in particular to a positioning control system installed on the toy aircraft. Background technique [0002] When the toy aircraft is in a hovering state in the air, sometimes it is hit by a crosswind, and at this time, the tail rudder of the toy aircraft will deviate in the horizontal direction. In order to correct this deviation phenomenon, the aeronautical flight system with strong anti-vibration performance that can adjust direction is usually installed on the tail rudder of toy aircraft. When the tail rudder of the toy aircraft deviates, the aviation flight system with strong shock resistance will send a corresponding control signal to the tail rudder servo on the toy aircraft, and the tail rudder will make the direction of the offset through the tail rudder Opposite action, thereby resisting the deflection of the rudder. [0003] In the prior art, the azimuth indicator of the toy aircraft is provided with...
Claims
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IPC IPC(8): A63H27/20A63H30/04
Inventor 马铿杰
Owner 马铿杰