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Aircraft control method, device and aircraft

A technology of flight control and control method, applied in the field of aircraft, can solve problems such as more difficult, limited orbital form, too harsh location shooting, etc., to achieve the effect of reducing requirements and breaking through limitations

Active Publication Date: 2021-11-26
SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, due to the natural limitations of the physical track, the laying of the track requires a good and flat terrain, which is too harsh for location shooting; limited space curve tracks like roller coaster tracks are even more difficult

Method used

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  • Aircraft control method, device and aircraft
  • Aircraft control method, device and aircraft
  • Aircraft control method, device and aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0072] image 3 It is a schematic flowchart of an aircraft control method provided by an embodiment of the present invention. The aircraft control method of the embodiment of the present invention can be implemented by the various components of the above-mentioned unmanned aerial vehicle in cooperation and is not limited here.

[0073] see image 3 , the aircraft control method includes:

[0074] Step 301, acquire information about space-constrained orbits.

[0075] Wherein, the information of the spatially constrained orbit may include parameters of an ordered sequence of spatial points.

[0076] The ordered spatial point sequence includes a plurality of spatial points arranged in sequence, and the parameters of the ordered spatial point sequence include the spatial position parameters of each spatial point in the ordered spatial point sequence.

[0077] The spatial location parameters may be spatial coordinates such as longitude, latitude and altitude.

[0078] refer to...

Embodiment 2

[0122] Figure 6 It is a schematic diagram of an aircraft control device provided by an embodiment of the present invention. Wherein, the device may be configured in the above-mentioned aircraft.

[0123] refer to Figure 6 , the aircraft control device includes:

[0124] Obtaining module 601, configured to obtain information about space-constrained orbits.

[0125] Wherein, the information of the spatially constrained orbit may include parameters of an ordered sequence of spatial points.

[0126] The ordered spatial point sequence includes a plurality of spatial points arranged in sequence, and the parameters of the ordered spatial point sequence include the spatial position parameters of each spatial point in the ordered spatial point sequence.

[0127] The spatial location parameters may be spatial coordinates such as longitude, latitude and altitude.

[0128] refer to Figure 4 , the space-constrained orbit can also be called the space virtual orbit, which is essenti...

Embodiment 3

[0177] Figure 7 It is a schematic diagram of the aircraft hardware structure provided by the embodiment of the present invention. The aircraft may be a drone or the like. Such as Figure 7 As shown, the aircraft includes:

[0178] fuselage 70;

[0179] The machine arm 71 is connected with the fuselage 70;

[0180] A power unit 711 is arranged on the machine arm 71;

[0181] one or more processors 701, located in the fuselage 70; and

[0182] A memory 702 connected in communication with the processor 701.

[0183] Figure 7 A processor 701 is taken as an example.

[0184] The processor 701 and the memory 702 may be connected via a bus or other means, Figure 7 Take connection via bus as an example.

[0185] The memory 702, as a non-volatile computer-readable storage medium, can be used to store non-volatile software programs, non-volatile computer-executable programs and modules, such as program instructions corresponding to the shooting control method provided by the ...

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PUM

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Abstract

The embodiment of the present invention discloses an aircraft control method, device, and aircraft, wherein the method includes: obtaining information on a space-constrained orbit; determining a space-constrained range according to the information on the space-constrained orbit; Command, determine the flight direction and flight speed in real time, and fly within the space constraint range according to the space constraint trajectory. The embodiment of the present invention imposes spatial curve position constraints on the aircraft equipped with cameras to form a space-constrained orbit, and realizes the effect of UAV track operation, which can break through the limitations of physical orbits, reduce the requirements for laying terrain conditions, and due to space constraints The track does not need to consider the versatility of disassembly and assembly, and it is completely possible to design a complex plane or space curve track form according to the shooting needs. In addition, the space-constrained track has no physical entity, which greatly improves the inconvenience in storage, transportation and use.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an aircraft control method, device and aircraft. Background technique [0002] In the shooting process of large-scale film and television works such as TV series, movies, advertisements, etc., the auxiliary shooting tool of photography track car is often used to achieve the effect of mobile shooting. The common camera and photography auxiliary equipment in life is a tripod, whose function is to fix the camera position, adjust the level, and facilitate the photographer to push, pull and pan. [0003] However, due to the natural limitations of the physical track, the laying of the track requires a good and flat terrain, which is too harsh for location shooting; Space curve tracks like roller coaster tracks are even more difficult. Contents of the invention [0004] In order to solve the above-mentioned technical problems, the present invention provides an aircraft control meth...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10G05D1/08
CPCG05D1/0808G05D1/101
Inventor 钟自鸣
Owner SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD