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Development and Flight Test of Unmanned Autonomous Rotor Navigation System Based on Virtual Instrumentation Platform

Virtual Instrumentation 플랫폼 기반 무인 자율 로터 항법시스템 개발 및 비행시험

  • 이병진 (건국대학교 항공우주정보시스템) ;
  • 박상준 (건국대학교 항공우주정보시스템) ;
  • 이승준 (건국대학교 항공우주정보시스템) ;
  • 김창주 (건국대학교 항공우주정보시스템) ;
  • 이영재 (건국대학교 항공우주정보시스템) ;
  • 성상경 (건국대학교 항공우주정보시스템)
  • Received : 2011.01.07
  • Accepted : 2011.06.14
  • Published : 2011.08.01

Abstract

The objectives of this research are development of guidance, navigation and control system for RUAV on virtual instrumentation and real flight test. For this research, the system is divided to DAQ (data acquisition) section, actuator section and controller section. And the hardware and software on each sections are realized on LabVIEW base. Waypoint guidance and control of auto flight are realized using PID gain tuning and waypoint vector tracking guidance algorism. For safe flight test, auto/manual switching module isolated from FCS (Flight Control System) is developed. By using the switch module, swift mode change was achieved during emergency flight case. Consequently, a meter level error of flight performance is achieved.

Keywords

Acknowledgement

Supported by : 한국연구재단

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Cited by

  1. Implementation of Virtual Instrumentation based Realtime Vision Guided Autopilot System and Onboard Flight Test using Rotory UAV vol.18, pp.9, 2012, https://doi.org/10.5302/J.ICROS.2012.18.9.878