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Boosting method, boosting device and tethered aircraft system of tethered aircraft

An aircraft and tethering technology, which is applied in the directions of ground devices, ground devices, and control/regulation systems for tethered aircraft, which can solve problems such as inability to reach the destination and achieve the effect of improving capabilities.

Active Publication Date: 2021-10-26
江苏网智无人机研究院有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a boosting method for tethered aircraft to solve the problem that the existing tethered aircraft cannot reach the target position due to the tension of the power supply rope in the horizontal direction when performing flight tasks

Method used

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  • Boosting method, boosting device and tethered aircraft system of tethered aircraft
  • Boosting method, boosting device and tethered aircraft system of tethered aircraft
  • Boosting method, boosting device and tethered aircraft system of tethered aircraft

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Embodiment Construction

[0020] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0021] The object of the present invention is to provide a boosting method for a tethered aircraft to solve the problem that the existing tethered aircraft cannot reach the target position due to the horizontal pulling force of the power supply rope when performing flight tasks.

[0022] The realization of the present invention is described in detail below in conjunction with specific accompanying drawing:

[0023] figure 1 A flow chart of the method for boosting a tethered aircraft provided in this embodiment is shown, and for ease of description, only parts related to this embodiment are shown. ...

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Abstract

A boosting method, a boosting device and a tethered aircraft system provided by the present invention, in the process of controlling the tethered aircraft to perform the flight mission, judge whether it is necessary to use the tethered aircraft according to the current position information and flight parameters of the tethered aircraft. During the flight mission, the tethered aircraft is provided with horizontal displacement thrust. If necessary, a control signal is generated according to the current position information and flight parameters, and then the tethered aircraft is controlled to generate horizontal displacement thrust, which overcomes the impact of the power supply rope on the tethered aircraft in the horizontal direction. The pulling force enables the tethered aircraft to reach the target position in the flight mission by overcoming the horizontal pulling force of the power supply rope during the execution of the flight mission, which improves the ability of the tethered aircraft to perform the flight mission.

Description

technical field [0001] The invention relates to the technical field of tethered aircraft, in particular to a boosting method, a boosting device and a tethered aircraft system for a tethered aircraft. Background technique [0002] As the use of aircraft or drones tends to become popular and entertaining, more and more aircraft or drone products on the market are sought after by consumers. A tethered aircraft is an aircraft including an aircraft main body, a power supply rope, and a ground power supply and control device. One end of the power supply rope is connected to the main body of the aircraft, and the other end is connected to the ground power supply and control device, and the ground power supply and control device provides electric energy for the aircraft main body through the power supply rope. Although the existing tethered aircraft pulls the power supply rope through the ground power supply and control device, and then controls the flying height and flight range o...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F3/02G05D1/10
CPCG05D1/10B64F3/02B64F3/00G05D1/0866
Inventor 不公告发明人
Owner 江苏网智无人机研究院有限公司