Forward flight speed and vertical speed matched patrol flight control method for unmanned helicopter

A technology of unmanned helicopters and forward flying speed, applied in the field of unmanned aerial vehicles, can solve the problems of unable to reach the target waypoint height, unmanned helicopters unable to complete line inspection tasks, etc.

Active Publication Date: 2015-04-29
NO 60 RES INST OF GENERAL STAFF DEPT PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the Δh / Δl between the two waypoints is small, the unmanned helicopter will first climb to the height of the target waypoint, and then level off; however, when the Δh / Δl between the two waypoints is large, the unmanned helicopter will first Reached the horizontal position of the target waypoint, but could not reach the altitude of the target waypoint
As a result, unmanned helicopters will not be able to complete line patrol tasks in some cases

Method used

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  • Forward flight speed and vertical speed matched patrol flight control method for unmanned helicopter
  • Forward flight speed and vertical speed matched patrol flight control method for unmanned helicopter
  • Forward flight speed and vertical speed matched patrol flight control method for unmanned helicopter

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Embodiment 1

[0025] This embodiment provides an unmanned helicopter's forward flight speed / vertical speed matching method for line patrol flight control, the structure is as follows: figure 1 , figure 2 as well as image 3 shown, including the following specific steps:

[0026] (1) According to Table 1, set the distance between the current position of the unmanned helicopter and the target waypoint to set the current forward flight speed v x is 7.0m / s, where the horizontal position difference Δl between the two waypoints is 400m, and the vertical height difference Δh is 300m;

[0027] (2) According to the forward flight speed v of the unmanned helicopter x , to determine the current vertical velocity v z The maximum and minimum values ​​of , according to can be calculated with the current forward speed v x Matched vertical velocity v z 5.25m / s;

[0028] (3) Calculation and current forward speed v x Matched vertical velocity v z , but cannot exceed the maximum and minimum vertic...

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Abstract

The invention discloses a forward flight speed and vertical speed matched patrol flight control method for an unmanned helicopter. The method comprises the following specific steps: (1), the current forward flight speed is set according to the current position of the unmanned helicopter and a target waypoint; (2), the maximum value and the minimum value current vertical speed vz are determined according to the forward flight speed vx of the unmanned helicopter; (3), if vz exceeds the limit, that is, when vz is smaller than VZmin or larger than VZmax, vz is equal to VZmin or VZmax, and vx is recalculated; (4), speed closed-loop control is performed respectively according to the acquired forward flight speed vx and vertical speed vz; and (5), height anomaly adjustment is performed. By means of the control method, the forward flight speed and the vertical speed of the unmanned helicopter are calculated in real time according to two waypoints as well as the current position and height information of the unmanned helicopter; the method is mainly applied to unmanned helicopter detection of a transmission line of a high-voltage line, an iron tower, a waste utility pole, an elevated antenna, a forest, a mountain and a hill under patrol, and line patrol work of the unmanned helicopter under complicated conditions is realized.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and relates to a line patrol flight control method for unmanned helicopter forward flight speed / vertical speed matching. Background technique [0002] While some developed countries in the world are actively investing in the development of unmanned helicopters, Chinese aviation industry workers are also working hard to develop their own unmanned helicopters. On September 29, 1993, China's first coaxial twin-rotor unmanned helicopter "Seagull" successfully made its maiden flight, marking that my country has overcome a series of corresponding technical difficulties. According to reports, the "Seagull" has a total weight of 300 kilograms and an engine power of 58.8 kilowatts. There is a flight control navigation system and a telemetry system on board, which can fly autonomously or remotely. This kind of helicopter can also be used in the military, and plays a special role in battl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
Inventor 王小青沈雯韩正伟张志清赵佳於拯威吴平冀明
Owner NO 60 RES INST OF GENERAL STAFF DEPT PLA
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