English  |  正體中文  |  简体中文  |  Items with full text/Total items : 56378/90242 (62%)
Visitors : 11684367      Online Users : 41
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
Scope Tips:
  • please add "double quotation mark" for query phrases to get precise results
  • please goto advance search for comprehansive author search
  • Adv. Search
    HomeLoginUploadHelpAboutAdminister Goto mobile version
    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/109565

    Title: Development of a Distributed Multi-MCU Based Flight Control System for Unmanned Aerial Vehicle
    Authors: Shiau, Jaw-Kuen;Hung, Wei-Sheng;Chang, Cheng-Min
    Keywords: Distributed Control System;State Feedback;Delay Compensation;UAV
    Date: 2015-09
    Issue Date: 2017-02-24 02:10:54 (UTC+8)
    Abstract: This paper presents the design of a distributed multi-microcontroller based computing framework for UAV application. A DSPIC microcontroller (MCU) based system architecture is established first. The system contains three major parts, namely, sensing and attitude determination section, control section, and ground section. The sensing and attitude determination section consists of four circuit boards (master control board, slave control board, sensor board, and power supply board) of identical size (5 cm × 5 cm). The sensor board contains three axes inertial measurement unit, electronic compass unit, and a GPS receiver. The sensors and the DSPIC MCUs are connected via an I^2C (inter-integrated circuit) data bus with the DSPIC of the master control board acting as the master MCU. Modular design was used to combine the master and slave control boards to form the system's control section and to facilitate system expansion for accommodating additional avionics functions. UART interface was used for inter-section communication. Results of the design and simulation of a model-based flight control system with time delay were also included to demonstrate the success of the design of the distributed multi-MCU based flight control system.
    Relation: Journal of Applied Science and Engineering 18(3), pp.251-258
    DOI: 10.6180/jase.2015.18.3.05
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Journal Article

    Files in This Item:

    File Description SizeFormat

    All items in 機構典藏 are protected by copyright, with all rights reserved.

    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - Feedback