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A method and device for determining flight time based on a multi-axis rotor UAV

A technology with unmanned rotors and a certain method, applied in the directions of measuring devices, instruments, measuring electricity, etc., can solve the problems of complex power consumption composition, large model size, and incomparable power consumption, and achieve the effect of prolonging the flight time.

Active Publication Date: 2018-11-27
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, this article involves a patent with a large model size and a symmetrical rotor distance of 35cm. It belongs to small and medium-sized UAVs, and the power consumption is not comparable.
In addition, the UAV designed in this paper is a system capable of aerial photography, and its power consumption not only includes the power consumption of the UAV, but the composition of power consumption is more complex.

Method used

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  • A method and device for determining flight time based on a multi-axis rotor UAV
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  • A method and device for determining flight time based on a multi-axis rotor UAV

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Embodiment Construction

[0051] specific implementation plan

[0052] The present invention is based on the airtime calculation method of the multi-axis rotor UAV, which is specifically realized through the following steps:

[0053] Step 1: Determine the relationship between the rotor speed of the UAV and the mass m of the aircraft;

[0054] Starting from the mechanical model of the aircraft, since the aircraft is mostly in the hovering state during the shooting process, the present invention takes the hovering state of the aircraft as the main research object. At this time, the pulling force of each propeller in the aircraft is equal, and the mechanical balance can be obtained:

[0055] L=G (1)

[0056] Among them, L is the pulling force of a single propeller, and the unit is N; G is the total gravity of the UAV; n is the number of propellers in the UAV. The propeller pulling force can be calculated by Abbott formula:

[0057] L=6.8×10 -17 ×D 3 ×p×n 2 (2)

[0058]Wherein, D represents the dia...

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Abstract

The invention discloses an endurance determination method and apparatus based on a multi-shaft rotor unmanned plane. A battery pack state of an aircraft is monitored and a real-time discharging current of the battery pack is collected; a voltage of the battery pack is measured; parameters of the current and the voltage and the like are processed, thereby obtaining an SOC of the battery pack; a wireless data transmission module is used for carrying out real-time data transmission and displaying the data on a ground terminal, thereby monitoring the SOC state of the battery all the time; and switching between parallel batteries is realized, so that the aircraft is in a mode above the electric quantity or voltage safety value level all the time. Endurance of the multi-shaft rotor unmanned plane is calculated based on the collected data and flight time of the aircraft under different parameters is also calculated. The method and apparatus have the following advantages: real-time calculation of flight time can be carried out according to a changing battery capacity and aircraft quality; and the flight time of the aircraft can be prolonged to the greatest extent.

Description

technical field [0001] The invention relates to a flight time calculation method, specifically, a method for determining flight time based on a multi-axis rotor UAV, mainly aimed at multi-rotor UAVs that are more suitable for use in the transportation field. technical background [0002] With the development of science and technology and the increase of military-to-civilian equipment, low-altitude unmanned aerial vehicles have been widely used in various civilian fields, such as geographic surveying and mapping, fire protection, public security, emergency response, marine monitoring, major disasters, etc. In terms of geographic surveying and mapping, drones are used to survey and map geographical and terrain conditions; in terms of emergency response, when major traffic accidents occur on urban roads, rescue vehicles and personnel cannot arrive at the scene of the accident in time, and drones are used to investigate and guide the accident scene , to obtain rescue information...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01R31/36G01R21/06
CPCG01R21/06G01R31/3646
Inventor 余贵珍张熙王云鹏徐永正孙伟力
Owner BEIHANG UNIV
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