Journal of Practical Engineering Education (실천공학교육논문지)

Korean Institute for Pratical Engineering Education (한국실천공학교육학회)
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A Study on Quadcopter Consisting of Dual Li-Po Battery Charging by Solar Cell in the Engineering Education Completed a Senier Project Work at the University

공학교육 이수체계에서 대학 졸업 작품용 이중 Li-Po 전원 사용 태양전지 충전 쿼드콥터 구성에 관한 연구

  • Yoon, Seong-Geun (Department of Electrical, Electronic & Control Engineering, College of Engineering, Kongju National University) ;
  • Kim, Kyung-Bin (Department of Electrical, Electronic & Control Engineering, College of Engineering, Kongju National University) ;
  • Chang, Eun-Young (Department of Electrical, Electronic & Control Engineering, College of Engineering, Kongju National University)
  • 윤성근 (국립 공주대학교 전기전자제어공학부 전자공학전공) ;
  • 김경빈 (국립 공주대학교 전기전자제어공학부 전자공학전공) ;
  • 장은영 (국립 공주대학교 전기전자제어공학부 전자공학전공)
  • Received : 2016.04.07
  • Accepted : 2016.04.26
  • Published : 2016.06.30
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Abstract

Depending on the college graduation project and graduation thesis regulations for the certification and graduation requirements, the quadcopter acting as a Li-Po battery that charges by solar energy are proposed a design method and improvements in theory. Quadcopter posture is balanced and confirmed by the position sensor, through a PID (Proportional Integral Differential) control. Battery switching circuit is composed of two Li-Po battery. Driving the quadcopter as one battery, and does not use other battery is charged by solar energy. A battery switching circuit is fabricated in a manner that uses two types of relays. Even if completely not charged to the battery is being driven a certain switch by the battery charging voltage from time to time, it proposes a method for increasing the endurance time and range.

졸업 조건 인증을 위한 졸업 작품 및 졸업 논문 제출 규정에 따라 설계/제작한 절차를 제시하고, 개선사항을 이론적으로 제안한다. 설계 내용은 태양 에너지로 충전시키는 Li-Po 배터리로 동작하는 쿼드콥터의 자세를 확인하고, PID(Proportional Integral Differential) 제어를 통하여 균형을 유지한 결과이다. 특히 2개의 Li-Po 배터리들을 탑재하고 태양 에너지를 이용하여 하나의 배터리를 충전시키는 동안에 다른 배터리로 구동하며, 배터리 전환 회로는 2종류의 릴레이들을 사용하여 배터리 전환 회로를 구성한다. 완전 충전되지 않았더라도 특정 전압으로 충전된 배터리를 구동중인 배터리와 수시로 절환시켜, 체공시간과 항속거리를 증가시키는 방법을 제안한다.

Keywords

References

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