Taxiing guide method

A technology for navigation aids and aircraft, applied in landing aids and other directions, can solve problems such as low efficiency, easy misunderstanding, and indistinguishable pilots, and achieve the effect of improving efficiency and being less misunderstood.

Inactive Publication Date: 2020-12-11
璞洛泰珂(上海)智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The existing airfield runway and taxiway centerline navigation lights are always on. Pilots can’t tell which navigation light they should taxi along. The tower and pilots frequently communicate with the pilot to guide the aircraft to taxi, which is inefficient and easy. misunderstood

Method used

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  • Taxiing guide method

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Embodiment Construction

[0018] 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.

[0019] see figure 1 , the present invention provides a technical solution: a sliding guidance method, comprising the following steps:

[0020] S1, the navigation light control system receives the data of the aircraft landing or departure;

[0021] S2, starting from the end of the runway, the scene monitoring system detects, calculates and updates the positions of the nose and tail of the aircraft, and obtains the position data of the aircraft;

[0022] S3, t...

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Abstract

The invention discloses a taxiing guide method. The taxiing guide method comprises the following steps of (S1) receiving aircraft landing or departure data by a navigation aid lamp control system; (S2) taking the runway terminal as a starting point, and detecting, calculating and updating the positions of the nose and tail of aircraft by a scene monitoring system so as to obtain aircraft positiondata; (S3) positioning center line navigation aid lamps which correspond to the nose and tail by the scene monitoring system, and sending positioning data to the navigation aid lamp control system fornext on-off control; (S4) controlling the front navigation aid lamps to automatically and successively turn on when the aircraft taxis by the navigation aid lamp control system; and (S5) sequentiallyturning off the back navigational lamps after the aircraft taxis. According to the taxiing guide method, the aircraft is guided to quickly and accurately taxi to the parking position from a runway ortaxi to the takeoff position from the parking position, frequent radio communication with a control tower is not needed, misunderstanding is not easy to generate, and the efficiency is improved.

Description

technical field [0001] The invention relates to the technical field of gliding guidance, in particular to a gliding guidance method. Background technique [0002] The existing airfield runway and taxiway centerline navigation lights are always on. Pilots can’t tell which navigation light they should taxi along. The tower and pilots frequently communicate with the pilot to guide the aircraft to taxi, which is inefficient and easy. misunderstood. Contents of the invention [0003] The purpose of the present invention is to provide a sliding guidance method to solve the problems raised in the background art above. [0004] In order to achieve the above object, the present invention provides the following technical solutions: a sliding guidance method, comprising the following steps: [0005] S1, the navigation light control system receives the data of the aircraft landing or departure; [0006] S2, starting from the end of the runway, the scene monitoring system detects, c...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/20
CPCB64F1/20
Inventor 潘东子朱江华沃尔夫冈·哈察克赵礼
Owner 璞洛泰珂(上海)智能科技有限公司
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