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An Analysis and Design Method of Continuous Descent Operation Program

A technology of operating procedures and design methods, applied in the field of civil aviation, to achieve the effect of simple and reliable technical solutions, satisfying real-time performance and high reliability

Active Publication Date: 2020-02-14
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Claims
  • Application Information

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Problems solved by technology

[0005] In order to solve the technical problems raised by the above-mentioned background technology, the present invention aims to provide an analysis and design method of a continuous descent operation program, overcome the shortcomings of the existing CDO program, and design a CDO program with certain advantages in energy saving, emission reduction and noise reduction. CDO program

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  • An Analysis and Design Method of Continuous Descent Operation Program
  • An Analysis and Design Method of Continuous Descent Operation Program
  • An Analysis and Design Method of Continuous Descent Operation Program

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Embodiment Construction

[0086] The technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0087] The analysis and design method of a kind of continuous descending operation program that the present invention proposes, the flow chart is as follows figure 1 shown, including the following steps:

[0088] Step 11, according to the initially designed CDO program, combine the navigation point coordinates and the database code table, consider the horizontal track and vertical profile, and establish an aircraft intention model;

[0089] Step 12, select a typical aircraft type, consider the uncertainty of aircraft quality and wind speed and direction, based on the aircraft particle model, combined with the above aircraft intention model, and use the aircraft basic performance database (BADA) to generate the aircraft's four-dimensional track;

[0090] Step 13, based on the above-mentioned generated series of four-dimensional aircraft tra...

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Abstract

The invention discloses a continuous descent operation program analysis and design method. The method comprises the following steps of: establishing an aircraft intention model according to an initially designed continuous descent operation program, a navigation point coordinate and a database encode table; selecting a typical type, considering the aircraft quality and the uncertainty of wind speed and wind direction, and generating an aircraft four-dimensional flight tracks on the basis of an aircraft particle model, the aircraft intention model and an aircraft basic performance database; and analyzing the distribution of heights and speeds of various aircrafts passing through waypoints under an uncertain condition and spacing distribution between the adjacent aircrafts during the matching between different types on the basis of a series of generated aircraft four-dimensional flight tracks, and judging whether the initial design of a CDO program is proper or not and whether the current control handover interval is reasonable or not, so as to guide the design and modification of the CDO program. According to the method disclosed by the invention, the disadvantages of the existing CDO programs are overcome, and CDO programs which have certain advantages in the aspects of energy saving, emission reduction and noise reduction are designed.

Description

technical field [0001] The invention belongs to the technical field of civil aviation, and in particular relates to an analysis and design method of a continuous descent operation program. Background technique [0002] In recent years, with the intensification of the energy crisis and the strengthening of environmental protection awareness, problems such as fuel consumption, airport noise, and exhaust emissions have become increasingly prominent. On the premise of safe operation, how to reduce fuel consumption as much as possible, alleviate airport noise, and reduce exhaust emissions have become the focus of attention of the civil aviation industry. The continuous descent operation procedure (Continuous Descent Operation, CDO) is based on the above background, and it was first proposed and applied in the developed countries of aviation. At present, the CDO technology in the United States, the Netherlands, Singapore and other countries is relatively mature, and it has been o...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F8/20G06F11/36
CPCG06F8/22G06F11/3608
Inventor 张军峰朱海波刘杰
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS