Correction control method for wing execution data of unmanned aerial vehicle
A control method and technology for unmanned aerial vehicles, applied in the field of unmanned aerial vehicles, can solve the problems of no obvious reference in the air, difficult adjustment, easy to be blown by gusts, etc.
Pending Publication Date: 2021-10-29
北京晟天行科技有限公司
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Problems solved by technology
[0005] The present invention provides a correction control method for the execution data of the UAV wing, which can effectively solve the problem that when the UAV is in the air without any obstruction, it is easy to be blown by the gust of wind and not Stable, and will deviate from the predetermined route of measurement, there is no obvious reference object in the air, difficult to adjust, and bring inconvenience to the measurement
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[0045] The terms "first" and "second" in the description and claims of the present invention and the above drawings are used to distinguish different objects, rather than to describe a specific order. Furthermore, the terms "comprising" and "having", as well as any variations thereof, are intended to cover a non-exclusive inclusion. For example, a process, method, system, product or apparatus comprising a series of steps or units is not defined by listed steps or units, but may include unlisted steps or units.
[0046] In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only It is an embodiment of the present invention, and those skilled in the art can also obtain other drawings according to the provided drawings w...
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The invention relates to a method for controlling the landing flight direction of an unmanned aerial vehicle, which is used for controlling the landing of the unmanned aerial vehicle when the unmanned aerial vehicle flies over multiple terrains and is characterized by comprising the following steps of: acquiring an acquired image when the unmanned aerial vehicle flies over the multiple terrains; identifying and detecting the acquired images when the unmanned aerial vehicle flies over the plurality of terrains, further acquiring data of a plurality of types of sensors mounted on the unmanned aerial vehicle, comparing and analyzing the identification and detection result and the sensor data, and controlling the landing flight direction of the unmanned aerial vehicle. According to the method for controlling the landing flight direction of the unmanned aerial vehicle, the problem of inaccurate image precision identification during current unmanned aerial vehicle landing control is avoided, the problems that dependence factors are single and environmental factors cannot be comprehensively analyzed during current landing control are solved. By integrating images and environmental factors, adaptive change landing control is carried out based on the specific condition of the current terrain environment, so that the flexibility and reliability of unmanned aerial vehicle control are improved.
Description
technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a method for correcting and controlling the execution data of the wings of the unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "unmanned aerial vehicle", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot, program control device, and signal acquisition device are installed. The personnel on the ground, on the ship, or at the remote control station of the mother aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. It can take off like an ordinary aircraft under radio remote control or launch into the air with a booster rocket, or it can be taken into the air by the parent aircraft to fly. Image tracking technology already exists in prior art drones,...
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Login to View More IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 王佩李帅
Owner 北京晟天行科技有限公司