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Instrument flight program three-dimensional design system

A technology for flight procedures and three-dimensional design, which is applied in the fields of instruments, calculations, special data processing applications, etc., and can solve problems such as unfavorable unified standards and popularization and application.

Active Publication Date: 2014-11-19
沈阳民航空管测绘设计有限公司
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  • Abstract
  • Description
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AI Technical Summary

Problems solved by technology

The application system in the flight procedure design industry presents a diversified status, which is not conducive to the unification of standards and promotion of applications

Method used

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  • Instrument flight program three-dimensional design system

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Embodiment Construction

[0018] Such as figure 1 As shown, a three-dimensional design system for instrument flight procedures. The system consists of five basic data management modules, two-dimensional automatic generation module of flight procedure protection area, automatic obstacle evaluation module, three-dimensional automatic presentation module of flight program protection area, and database module. It is composed of modules, among which the two-dimensional automatic generation module of flight procedure protection zone can generate flight procedure protection zones that comply with relevant ICAO specifications and meet the requirements of 3σ safety probability, including traditional instrument flight procedure two-dimensional protection zone and PBN instrument flight procedure two-dimensional protection Area; the obstacle automatic evaluation module can call the data in the basic data management module of the system, realize automatic obstacle evaluation of the generated flight procedure protecti...

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Abstract

The invention relates to an instrument flight program three-dimensional design system which is composed of a system basic data management module, an automatic flight program protection area two-dimensional generation module, an automatic obstacle evaluation module, an automatic flight program protection area three-dimensional presenting module and a database module. The automatic obstacle evaluation module can be used for calling data in the system basic data management module, achieving automatic obstacle evaluating on a generated flight program protection area, a navigation facility shielding surface and the like and sending an evaluation result to the automatic flight program protection area two-dimensional generation module to check whether the flight program protection area can keep the specified safety margin on obstacles. The automatic flight program protection area three-dimensional presenting module is used for conducting three-dimensional dynamic presenting on the flight program two-dimensional flight program protection area and the like. The instrument flight program three-dimensional design system can be used for achieving the functions of automatically generating the flight program protection area, automatically evaluating the obstacles and conducting three-dimensional presenting and perpendicular exaggerating on the flight program protection area and a high-precision mass DEM database and the like.

Description

Technical field [0001] The invention relates to an instrument flight procedure three-dimensional design system, which is used for two-dimensional automatic generation, obstacle automatic evaluation and three-dimensional automatic presentation of flight procedure protection zones, and uses high-precision massive DEM data to verify flight procedure protection zone drawing in a three-dimensional environment The rationality and correctness of the results and evaluation conclusions belong to the field of computer application technology. Background technique [0002] Flight procedure design is a method of planning approach and departure. The purpose is to straighten out the relationship between the route and landing or take-off. It is an important measure to ensure flight safety and prevent aircraft from colliding with ground obstacles. The flight safety of aircraft plays an extremely important role. [0003] After the mid-1980s, with the development of CAD technology and electronic map...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 李斌郭兆宏黎新徐国标刘本勇郭明伟王雨杨海彬孙寅寅姜庆昱关昕戴雯思刘飞樊海舰张滢
Owner 沈阳民航空管测绘设计有限公司
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