Aircraft landing monitoring guiding system

A guidance system and aircraft technology, applied in the field of guidance systems, can solve various problems such as fixed parameters, inability to move, affecting flight safety, etc., and achieves the effects of expensive equipment, convenient disassembly and assembly, and simple maintenance.

Active Publication Date: 2017-05-31
NAVAL AVIATION UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] There are three problems with the installation of the centerline camera: first, the new airport needs to be pre-installed and cannot be moved; second, the relevant parameters are fixed and cannot be adjusted flexibly; flight safety

Method used

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  • Aircraft landing monitoring guiding system
  • Aircraft landing monitoring guiding system
  • Aircraft landing monitoring guiding system

Examples

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Embodiment Construction

[0030] The specific embodiment will be further described below in conjunction with the accompanying drawings:

[0031] 1. System settings

[0032]The system consists of a monitor, a control computer and a camera. When the training runway is selected, an ideal landing point should be set on the runway. According to the actual situation of the aircraft runway 1 on board, determine the center point between the second and third arresting cables as the ideal landing point; for this reason, set it as the ideal landing point on the determined aircraft 1 runway about 500 meters away from the start of the runway The location of the landing point; after determination, draw an obvious horizontal line on the runway vertical to the center line of the runway, which represents the center line between the second and third arresting wires of the ship's landing runway; from the center line as the starting point to the aircraft 1 direction, measure the distance from the centerline between the ...

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Abstract

The invention relates to an aircraft landing monitoring guiding system. According to the aircraft landing monitoring guiding system, firstly, an ideal landing point, a stern line and a runway finishing line are set on a runway; secondly, a camera (6) is selected and is mounted outside the runway at one side of a transverse line of the runway finishing line, a view center of the third camera (6) aligns a far-end point of an ideal glide path; an optical landing assisting system (5) is mounted outside the runway at a same side as the camera (6); a commander (2) and a monitor (3) are at same side of the runway as the camera (6) and the optical landing assisting system (5); the camera (6) is connected with a control computer (4) and a monitor (3) through signal wires; a whole flight process of an aircraft (1) along the ideal glide path is observed by the commander (2), images of the aircraft (1) during gliding flight are acquired from the monitor (3); high-low and left-right deviation of the aircraft (1) is determined by the commander (2), and a pilot is prompted to land the aircraft (1).

Description

technical field [0001] The invention belongs to the field of aviation flight support, and in particular relates to a guidance system for monitoring and directing the flight situation of the aircraft during the landing process of the aircraft. Background technique [0002] During the landing training of the fixed-wing carrier-based aircraft, since the landing runway of the aircraft carrier is very short, the pilot must control the aircraft to slide down the ideal glideslope during the process of the aircraft sliding down the glideslope. If it cannot glide along the ideal glideslope, the aircraft will land If the point is too close, too far, or deviates from the airstrip, a go-around, escape, or even a hard landing will occur; therefore, directing an aircraft to land on an aircraft carrier is a specialized knowledge that requires long-term training. In order to ensure that the fixed-wing carrier-based aircraft glides down the ideal glideslope, the precise command of the landin...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G08G5/02
CPCG08G5/025
Inventor 李喜龙林本龙王月基陈强姜鹏王文华崔焰王涛张威孙洪波王发龙
Owner NAVAL AVIATION UNIV
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