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The Design and Realization of Embedded Flight Control System for SUAV Based on ARM

Author: MeiXianLin
Tutor: CaoYunFeng
School: Nanjing University of Aeronautics and Astronautics
Course: Navigation,Guidance and Control
Keywords: Tiny unmanned aerial vehicles Flight Control System ARM Attitude determination system Bootloader
CLC: V227
Type: Master's thesis
Year: 2008
Downloads: 244
Quote: 3
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Abstract


Of this topics stems from the aerial robot contest the competition project . Against the the competition requirements , put forward a the low-cost of the one kinds ARM-based , the the overall program of the the high-performance embedded tiny unmanned aerial vehicles flight control system , and thus giving rise to a a series of of the research the work of of . The the the focus of of this article is to the the the posture of of the flight control system determine the the the design and realization of of of the system design and the the hardware of the flight control system of the . The The The of this article First of all Recalling the a the at home and abroad tiny unmanned aerial vehicles course of development of , to introduces the its research the status quo , and pointed out that the a the trend of the tiny unmanned aerial vehicles the development of . According to the demand for design a low-cost -bit , the the overall program of the the high-performance embedded tiny unmanned aerial vehicles flight control system . Design a determine the system program for the the posture of the the tiny unmanned aerial vehicles of the the in low-cost , low- power consumption of the and , take advantage of the posture four yuan the number of , Runge-Kutta method , Gaussian Newton method and expansion Kalman filter is estimated the the the posture of of the out of the system matrix ; on the the attitude determination the program carried out a simulation . Design a the the hardware of the the the flight control of system of of the based on the ARM part of the , including the power supply and reset circuit , the the interface circuit of the UART , SPI, JTAG , and , etc. , PWM signal occurrence of circuit , the A / D sampling circuit , and pre- circuit , photoelectric coupling circuit, etc. ; completed the the entire the PCB board production , system of the the flight control as well as on the by the design the of the debugging the work of of the circuit , makes the the operation of the system to normal . Finally against the the carried out startup code , etc. the the preparation of of the system the underlying software and debugging to the the hardware platform of the of this article design of , the establishment of a of the boot environment of the system .

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