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Guidance landing system for aircraft horizontal trajectory ship landing mode, and method thereof

A horizontal track and aircraft technology, applied in control/adjustment systems, landing aids, 3D position/channel control, etc. The effect of flight safety factor, reducing psychological pressure and operation difficulty, reducing physical strength and energy effort

Active Publication Date: 2018-11-13
陈穗
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the above-mentioned process, due to the long landing process and the slanted flight path, the flight is more difficult. The pilot needs to be highly concentrated, pay more physical strength and energy, and the psychological pressure will be greater. The difficulty factor of flight safety larger

Method used

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  • Guidance landing system for aircraft horizontal trajectory ship landing mode, and method thereof
  • Guidance landing system for aircraft horizontal trajectory ship landing mode, and method thereof

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Embodiment Construction

[0024] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0025] The purpose of the present invention is to provide a guided landing system and method of aircraft horizontal track landing mode, to solve the problems existing in the prior art, reduce the difficulty factor of aircraft landing on ships, and improve the flight safety factor.

[0026] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in c...

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Abstract

The invention discloses a guidance landing system for an aircraft horizontal trajectory ship landing mode, and a method thereof. The guidance landing system comprises a green signal lamp, an orange signal lamp, a red signal lamp and a rangefinder which are arranged on a ship deck. The green signal lamp is arranged at the tail of the ship deck. The orange signal lamp, the red signal lamp, the rangefinder and the green signal lamp are sequentially arranged on the deck. The rangefinder is electrically connected with the red signal lamp through a controller. An aircraft landing point is located between the green signal lamp and the orange signal lamp. According to the guidance landing system for the aircraft horizontal trajectory ship landing mode, and the method thereof, the easier-to-operatetrajectory of the aircraft landing on the ship is put forward, and through guidance of the guidance landing system for the aircraft horizontal trajectory ship landing mode, the difficulty coefficientof aircraft landing is decreased, physical strength and energy effort of an aviator is reduced, the psychological pressure borne by the aviator and the operation difficulty are reduced, the flight quality is improved advantageously, and the flight safety factor is increased advantageously.

Description

technical field [0001] The invention relates to the technical field of guiding an aircraft to land, in particular to a system and method for guiding an aircraft to land in a horizontal track landing mode. Background technique [0002] The flight mode of the existing aircraft landing on the ship is to land on a slow landing track at an angle of 4° with the sea level, chasing the ship sailing at a constant speed and finally landing on the deck of the ship. In the process of chasing and descending, using the guiding device combined with Fresnel lens, the aircraft will realize the slow landing with an included angle along the parallel beam path given by the Fresnel lens. [0003] In the above-mentioned process, due to the long landing process and the slanted flight path, the flight is more difficult. The pilot needs to be highly concentrated, put in more physical strength and energy, and the psychological pressure will be greater. The difficulty factor of flight safety larger. ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/20G05D1/10
CPCB64F1/20G05D1/101
Inventor 陈穗
Owner 陈穗
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