Method for designing flight parameter system with comprehensive alarm function

A flying parameter system and design method technology, applied in the field of avionics, can solve the problems of corresponding search, reduce cross-linking relationship, difficult flying parameter data, etc., and achieve the goal of reducing cost and weight, reducing cross-linking relationship and improving maintainability Effect

Active Publication Date: 2020-03-24
SHAANXI QIANSHAN AVIONICS
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AI Technical Summary

Problems solved by technology

[0006] Solve the problem that the cause of the alarm is difficult to find correspondingly with the flight parameter data during the flight training process

Method used

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  • Method for designing flight parameter system with comprehensive alarm function
  • Method for designing flight parameter system with comprehensive alarm function
  • Method for designing flight parameter system with comprehensive alarm function

Examples

Experimental program
Comparison scheme
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Embodiment

[0030] The following takes the implementation of the flight reference system of an aircraft as an example to describe the implementation process:

[0031] 1. Design a general-purpose hardware platform. The hardware platform is configurable. According to the requirements of the flight parameter collection configuration file and the alarm output configuration file, the corresponding flight parameter collection and alarm information output are carried out;

[0032] 2. According to the needs of users, compile the flight parameter collection configuration file and alarm output configuration file supporting this model: the flight parameter collection configuration file and alarm output configuration file are the support of the entire general design. The hardware platform has the ability to accept configuration files. By identifying the configuration file for flight parameter acquisition, the acquisition module of the flight parameter collector can collect the data of the aircraft sub...

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Abstract

The invention relates to a method for designing a flight parameter system with a comprehensive alarm function, belongs to the field of computer automatic control, and is applied to the technical fieldof avionics. The invention relates to designing of a flight parameter system with a comprehensive alarm function, hardware is a universal platform, and software is divided into an airborne part and aground part. The airborne part is a universal software module, the realized functions of the airborne part are set by a flight parameter acquisition configuration file and an alarm output configuration file, and the design mode can be applied to output control of various alarm signals on an airplane, such as light alarm, voice alarm, picture alarm and the like. According to the invention, a flight parameter acquisition recording function and a comprehensive alarm function are fused, the problem that the alarm reason is difficult to find in the flight training process is solved, the aircraft maintainability is improved, and the cost and the weight are reduced.

Description

technical field [0001] The invention belongs to the category of computer automatic control and is applied in the technical field of avionics. Background technique [0002] The number of systems and components included in the aircraft system is very large, ranging from avionics, flight control, hydraulic pressure, fuel, environmental control, landing gear, power supply and other systems to various valves, pumps and motors. various parts of the aircraft. The flight parameter collector generally collects the signals of each system and sends them to the recording device for recording. Through data download and playback, the ground inspection and maintenance capabilities of the aircraft are improved, and the alarm system is used to collect the faults of each system during the flight. \Status information, prompting the pilot to take action. [0003] At present, the alarm system uses the integrated alarm as the core equipment to drive the alarm device. The data required by the in...

Claims

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Application Information

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IPC IPC(8): G07C5/08G06F30/15
CPCG07C5/0841G07C5/0808G07C5/0816Y02T90/00
Inventor 白皓董鹏辉杨毅
Owner SHAANXI QIANSHAN AVIONICS
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