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Design and Implementation of the Kitty Hawk the -500 aircraft landing gear fault diagnosis system

Author: NiuBingHui
Tutor: HuangXianHe；PengWeiDong
School: University of Electronic Science and Technology
Course: Software Engineering
Keywords: Aircraft landing gear Retraction system Failure Analysis Fault Diagnosis B / S architecture
CLC: V226
Type: Master's thesis
Year: 2010
Downloads: 117
Quote: 0
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Abstract


The landing gear system is one of the key components of the aircraft , due to the relatively poor working environment , a higher probability of failure in the use of their work performance directly affect the takeoff and landing performance and flight safety . The actual repair analysis and research for the failure of the landing gear system , mainly using artificial judgment , this approach is not only low efficiency and strong subjective experience particularly strong dependence , this method has not to meet the needs of existing maintenance . Firstly, a detailed analysis of the working principle and structure of the Kitty Hawk aircraft landing gear systems , in-depth study of its retraction system , then the basis of further analysis of common failure to establish the equations of motion of the retractable institutions in the ideal state of movement lazytongs simulation and Pro / E environment , put down the device exists went on emergency the existing lazytongs in , analyze , and propose modifications recommended to complete the design of the modified system principle . Starting from the structure and working principle of the aircraft landing gear systems , common failure analysis in the basis of the traditional fault diagnosis , fault diagnosis system design . According to the method of software engineering , process analysis , the proposed design of the functional requirements , and operating environment of the system 's hardware and software design , system ER ( relationship entity diagram ) , PowerDesigner tool to establish the conceptual model of the database to meet the design needs and physical model , and generate the corresponding MS SQL SERVER database table . Based on the above design , NET platform - based development techniques , Kitty Hawk the -500 aircraft landing gear fault diagnosis system based on B / S structure and the corresponding test . The system interface is friendly, easy to operate , powerful , able to meet the current needs of the system .

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CLC: > Aviation, aerospace > Aviation > Aircraft Construction and Design > Landing gear
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