한국해양대학교

Detailed Information

Metadata Downloads

레이저렌지파인더를 활용한 무인항공기의 자동회피 시스템

DC Field Value Language
dc.contributor.author 김현 -
dc.date.accessioned 2017-02-22T06:01:45Z -
dc.date.available 2017-02-22T06:01:45Z -
dc.date.issued 2013 -
dc.date.submitted 57016-04-17 -
dc.identifier.uri http://kmou.dcollection.net/jsp/common/DcLoOrgPer.jsp?sItemId=000002174863 ko_KR
dc.identifier.uri http://repository.kmou.ac.kr/handle/2014.oak/8976 -
dc.description.abstract As the technology of air force industry develops the invention of automatic aircraft was possible, which is a plane with no person on air -
dc.description.abstract the pathways that the aircraft is succeeding is departed to 5 directions. When the barrier is detected in the pathways of an automatic aircraft, the MCU which is located in the inner structure of the craft decides the safest avoiding direction according to the area that is detected with the obstacle and the direction of progress of the airplane. When it decides the direction to evade, the auto-craft sends a PWM signal which can move itself away from the obstacle. It is structured a LabVIEW system which users can simultaneously check the flight conditions live from a PC from using a Zigbee wireless communication. Not only that, while the craft is evading, it is designed to return to the previous track after the avoiding progress by enforcing counting to a certain function. -
dc.description.abstract using Laser Range Finer (LRF). In this thesis the area that is detected of obstacles by using LRF is divided by 3 directions -
dc.description.abstract remote controlling the craft for afar. Moreover, these days with the introduction of automatic navigating systems, it made far distance and auto flights possible. The automatic navigation system is a term which the plane flies to the destination through received pathways and information in advance. When the plane discovers an obstacle while flying its path, it needs an obstacle filtering system that can sense the obstacle and therefore avoid it. The existing detecting system is a method that uses infrared light sensors, however, is vulnerable to sun rays and short detecting distances. The research regarding automatic aircraft has been prioritizing it safety due to dangers of possible accidents. In this research it supplemented the disadvantages of previous methods and suggests a new automatic dodging system that is free of sun rays and has long detecting distances -
dc.description.tableofcontents Abstract 그림 목차 표 목차 1장 서론 2장 무인항공기 2.1 무인항공기의 특성 2.2 무인항공기의 동작 2.2.1 호버링 제어 2.2.2 롤, 피치 제어 2.3 무인항공기의 구성 2.3.1 APM2 제어부 2.3.2 모터부 2.3.3 장애물 검출부 3장 무인항공기의 제어 3.1 레이저 렌지 파인더 3.1.1 레이저 렌지 파인더의 특성 3.1.2 레이저 렌지 파인더의 동작 3.2 레이저 렌지 파인더를 사용한 회피시스템 3.2.1 회피시스템의 구성 및 동작 3.2.2 회피시스템의 알고리즘 3.2.3 PWM 제어 4장 실험 및 결과 4.1 실험 환경과 설정 4.2 LabVIEW 모니터링 결과 4.3 APM2에서의 PWM데이터 분석 5장 결론 참고문헌 -
dc.language kor -
dc.publisher 한국해양대학교 -
dc.title 레이저렌지파인더를 활용한 무인항공기의 자동회피 시스템 -
dc.type Thesis -
dc.date.awarded 2013-08 -
Appears in Collections:
전자통신공학과 > Thesis
Files in This Item:
000002174863.pdf Download

Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.

Browse