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Method and device for evaluating collision rate of aircraft in continuous descent based on the idea of ​​aircraft pairing

A collision rate and aircraft technology, applied in aircraft traffic control, three-dimensional position/airway control, vehicle position/route/altitude control, etc., which can solve the lack of safety assessment work for continuous descent and arrival procedures, and difficulty in controlling flight accuracy, etc. question

Active Publication Date: 2021-12-17
中国民航管理干部学院 +2
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Problems solved by technology

However, during this process, the flight accuracy is difficult to control because the aircraft uses slow thrust to descend. In order to ensure flight safety and improve flight efficiency, the air traffic control system (ATC) needs to reasonably control the safety risks during the descent process.
[0003] In the existing research, the collision rate evaluation of aircraft is mainly aimed at the cruising process or the traditional ascending and descending process, and the safety evaluation work for the continuous descending and arriving procedures is relatively scarce.

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  • Method and device for evaluating collision rate of aircraft in continuous descent based on the idea of ​​aircraft pairing
  • Method and device for evaluating collision rate of aircraft in continuous descent based on the idea of ​​aircraft pairing
  • Method and device for evaluating collision rate of aircraft in continuous descent based on the idea of ​​aircraft pairing

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Embodiment Construction

[0030] The technical solutions of the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0031] The aircraft continuous descent collision rate evaluation method provided by the present invention is realized based on the idea of ​​aircraft pairing, and mainly studies the collision rate of aircraft descending along the same route in a fixed scene. A pair of aircraft refers to two aircraft on the same route, the aircraft in front is called the leading aircraft, and the aircraft behind is called the trailing aircraft. The aircraft continuous descent collision rate assessment method provided by the present invention: for aircraft of different aircraft types, establish vertical continuous descent flight path models respectively, and utilize the optimal control method to predict the vertical continuous descent flight path according to the state of the aircraft; The predicted vertical continuous descent...

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Abstract

The invention discloses a method for evaluating the collision rate of aircraft continuous descent, which comprises the following steps: S1, determining the arrival rate of aircraft, the number of aircraft and the type of aircraft in the scene to be evaluated; S2, according to the type of aircraft, calculating the vertical S3, enumerates all aircraft pair combinations; S4, according to the vertical continuous descent flight path, respectively calculates the relationship curves between the travel time and travel distance of the leading aircraft and the trailing aircraft in the aircraft pairing, and calculates the The collision rate of the aircraft pair; S5, calculate the continuous descending collision rate of all the aircraft pairs in the scene to be evaluated. The aircraft continuous descent collision rate evaluation method provided by the present invention is realized based on the idea of ​​aircraft pairing, and can calculate the vertical continuous descent track of the aircraft according to different descent conditions, and use the track data to estimate the collision rate in the terminal area descent stage. The present invention also discloses a device for realizing the above evaluation method.

Description

technical field [0001] The invention relates to a method for evaluating the collision rate of a continuous descent of an aircraft, and at the same time relates to a device for realizing the method for evaluating the collision rate of a continuous descent of an aircraft. Background technique [0002] Approach refers to the process in which the aircraft is aligned with the runway when it descends. In the approach phase, to adjust the altitude of the aircraft and align it with the runway, so as to avoid ground obstacles, the pilot must concentrate on the operation accurately. Recently, there are strict standards and operating procedures. The continuous descent approach (Continuous Descent Approach / Arrival, CDA) used by the aircraft during the descent can reduce fuel consumption, reduce exhaust emissions, and reduce noise pollution. However, during this process, the flight accuracy is difficult to control because the aircraft descends with idle thrust. In order to ensure flight...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G08G5/04G05D1/10
CPCG08G5/04G05D1/1064
Inventor 管祥民吕人力于一胡疋盈
Owner 中国民航管理干部学院