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Aircraft track self-adaptive planning method, device and equipment and storage medium

An aircraft, self-adaptive technology, applied in the direction of instruments, three-dimensional position/course control, vehicle position/route/altitude control, etc., can solve the problems of long working time, low efficiency and long cycle time of aircraft, and reduce turning The effect of staying and waiting time and improving work efficiency

Pending Publication Date: 2021-11-05
PRODRONE TECH (SHENZHEN) CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The technical problem to be solved by the present invention is to solve the problem that the execution cycle time of the aircraft trajectory planning method in the prior art is long, resulting in a long execution time of the aircraft and low efficiency.

Method used

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  • Aircraft track self-adaptive planning method, device and equipment and storage medium
  • Aircraft track self-adaptive planning method, device and equipment and storage medium
  • Aircraft track self-adaptive planning method, device and equipment and storage medium

Examples

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Effect test

Embodiment 1

[0049] Such as figure 1 As shown, when the aircraft performs some tasks such as route inspection, plane surveying and mapping, and 3D modeling, it needs to navigate autonomously and guide the trajectory. Generally, track planning is carried out in the form of point-to-point. After arriving at the point, turn to the next point by fixed-point steering, and reciprocate to realize the entire trajectory planning process. After arriving at the point, a fixed-point turn or a waiting coordinated turn is required. E.g figure 1 From 0 o'clock to 1 o'clock to 2 o'clock in the form of point-to-point, after 1 o'clock, turn to 2 o'clock through a fixed point, this method is not very efficient, and there will be deceleration, pause and waiting after the point ,low efficiency. Based on the above defects, the present invention provides a method for adaptive track planning, such as figure 2 As shown, from 0 o'clock to 1 o'clock to 2 o'clock is the way of adaptive coordinated turning. In the...

Embodiment 2

[0065] Based on Embodiment 1 of the present invention, Embodiment 2 of the present invention also provides a device for adaptive planning of a track, including:

[0066] Relational model, used to construct the relationship between the pitch angle, roll angle and azimuth angle of the aircraft;

[0067] The coordinated turning condition acquisition module is used to acquire the coordinated turning condition that the roll angle needs to meet when the aircraft performs an azimuth turn;

[0068] The flight trajectory equation building block is used to construct the differential equations that the flight trajectory of the aircraft needs to satisfy;

[0069] The flight trajectory acquisition module is used to segmentally input the pitch angle, roll angle, azimuth angle, vertical axis speed, latitude, longitude, and altitude that meet the coordination turning conditions and the relationship between the pitch angle, roll angle, and azimuth angle Substituting the differential equations...

Embodiment 3

[0083] Based on Embodiment 1 of the present invention, Embodiment 3 of the present invention also provides an electronic processing device, including at least one processor and a storage device storing at least one execution program, when the at least one execution program is executed by the at least one processor Executing, the at least one processor implements the method as described above.

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Abstract

The invention relates to an aircraft track adaptive planning method, device and equipment and a storage medium. The method comprises the following steps: constructing a relational expression among a pitch angle, a roll angle and an azimuth angle of an aircraft; obtaining a coordinated turning condition which needs to be met by a roll angle when the aircraft performs azimuth turning; constructing a differential equation set which needs to be met by the flight path of the aircraft; inputting and substituting the pitch angle, the roll angle, the azimuth angle, the longitudinal axial speed, the latitude, the longitude and the height which meet the coordinated turning condition and the relational expression among the pitch angle, the roll angle and the azimuth angle in a segmented mode into a differential equation set which needs to be met by the flight track of the aircraft to obtain track parameters, and therefore segmented tracks are established; and fitting each segmented track to obtain a final flight track of the aircraft, and enabling the aircraft to move according to the flight track. The method has the advantages that the working execution time of the aircraft is shortened, and the efficiency is high.

Description

technical field [0001] The present invention relates to the technical field of UAV flight management and control, in particular to a method, device, equipment and storage medium for adaptive planning of aircraft track. [0002] technical background [0003] Unmanned multi-rotor aircraft usually perform some autonomous tasks, such as route inspection, plane surveying, three-dimensional modeling, etc., and performing these tasks requires autonomous navigation and guidance for the trajectory. The general trajectory planning is carried out in the form of point-to-point. After arriving at the point, it turns to the next point by fixed point, and realizes the whole trajectory planning process in this way. This method is not very efficient in terms of efficiency. There will be deceleration, pause and waiting after the point is reached. For some scenes where there is no action at the point, such as farmland spraying, isochronous and equidistant photography, path tracking and other ap...

Claims

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Application Information

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IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/106
Inventor 黄立张正飞洪亮张原艺王龙薛源刘华斌吴春兰
Owner PRODRONE TECH (SHENZHEN) CO LTD
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