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The Design and Analysis of Flight Management Simulation System

Author: MengFanPeng
Tutor: JingZhongLiang；HuShiQiang
School: Shanghai Jiaotong University
Course: Control Theory and Control Engineering
Keywords: Flight Management System Simulation Embedded Systems Linux Driven Development
CLC: V243
Type: Master's thesis
Year: 2011
Downloads: 188
Quote: 1
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Abstract


Flight Management System (Flight Management System) is a civil aircraft avionics system is the core system . FMS can pilot pre- flight planning and navigation input database generation flight path , and make the aircraft along the flight path , but also can be used with air traffic management , airborne collision avoidance system , terrain awareness and warning system, through information exchange and other changes in flight track to re- navigate and optimization. FMS the aircraft throughout the flight has a crucial role in modern aircraft safety , automation, economy flight has an irreplaceable role . This paper focuses on the FMS simulation technology has been studied to build a flight management simulation system (Flight Management Emulation System FMES). First constructed in the embedded system development board running with the core functionality of FMS flight management module , on the basis of the provisions in the agreement to build a FMES the display and control module , two modules interconnected via ARINC429 bus , complete transfer of data between two modules . To complete the main work focuses on FMES the display and control module and data communication module , and finally integrates the entire system. The main contents are as follows : ⑴ analyzed ARINC702 stipulated in the agreement of FMS core functions and interfaces proposed flight management simulation system and gives the overall framework of the hardware and software frameworks. ⑵ analysis based on interface design and implementation of simulation of FMS display and control module, which completed a man-machine interface functions and flight management function module execution environment , the formation of closed-loop simulation FMS provides a runtime environment and operation of the module interface. ⑶ selected a POWERPC Series development board and the development board provides PPCLinux operating system elaborated simulation FMS modules. ⑷ ARINC429 selected two commercial communication board , completed data between two communication modules . The module is implemented using a hierarchical structure in a PPC Linux environment, were used to develop the USB driver layer 429 protocol layer and the data transmission board layer .

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CLC: > Aviation, aerospace > Aviation > Aircraft instrumentation,avionics, flight control and navigation > Electronic equipment
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