Aircraft safety take-off control method and device

A control method and control device technology, applied in the field of aircraft, can solve problems that affect the smooth take-off of the aircraft, inaccurate judgment, etc.

Inactive Publication Date: 2015-07-22
SHENZHEN AEE AVIATION TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It can be seen from this that in the current technology, judging whether the aircraft is in a horizontal position by naked eyes may easily lead to ina

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  • Aircraft safety take-off control method and device
  • Aircraft safety take-off control method and device
  • Aircraft safety take-off control method and device

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Embodiment Construction

[0029] It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.

[0030] The present invention provides a method for controlling the safe take-off of an aircraft, referring to figure 1 , in one embodiment, the aircraft safety take-off control method includes:

[0031] S10. Acquire angle information between the aircraft body and the horizontal plane through an angle sensor.

[0032] The angle sensor is a three-axis gyroscope, through which the angular velocity of the aircraft in four directions on the horizontal plane can be measured simultaneously. The angle sensor is arranged in the middle of the aircraft fuselage, and the angle information between the aircraft fuselage and the horizontal plane is measured by the angle sensor.

[0033] Specifically, before the aircraft is placed on the ground or other planes and ready to take off, the angle information between the aircraft ...

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Abstract

The invention discloses an aircraft safety take-off control method. The method comprises the steps of 10, obtaining information of an angle between an aircraft body and the horizontal plane through an angle sensor; 20, judging whether the obtained information of the angle is smaller than or equal to the maximum safety angle threshold value or not; 30, controlling the aircraft to take off if the obtained information of the angle is smaller than or equal to the maximum safety angle threshold value. The invention further discloses an aircraft safety take-off control device. By the adoption of the technical scheme, whether the aircraft is horizontally placed or not can be accurately judged, and the aircraft can safely take off.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a method and device for controlling the safe take-off of an aircraft. Background technique [0002] A flight vehicle is an instrumental flying object that is made by humans, can fly off the ground, fly in space, and be controlled by humans in the atmosphere or in outer space (space). The aircraft includes unmanned aerial vehicles, etc., which can fly in automatic flight mode, manual flight module or semi-automatic flight mode to complete aerial photography or reconnaissance affairs. Before the aircraft takes off, it must be placed on the ground or other planes to take off; during the take-off process, the software and hardware of the aircraft start to work, the power motor of the aircraft starts to rotate at a high speed, the state of the whole aircraft changes greatly during take-off, and the external Due to the influence of the environment (such as wind, etc.), the take-off failure or ...

Claims

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Application Information

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IPC IPC(8): B64D47/02G05D1/00
Inventor 张显志
Owner SHENZHEN AEE AVIATION TECH
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