원문정보
초록
영어
In this paper, Fly robot with electric power, a kind of Unmanned aerial vehicle (UAV), is considered as an autonomous hovering platform, capable of vertical lift-off, landing and stationary hovering. This aircraft has four rotor and DC motors of electrical Power, which is capable of Omni-direction for indoor application. In the earlier days of vertical flight experimentation developers looked at the intuitively easy control functionality of 4 rotor designs. But we need to obtain design method of suitable structures and adequate components because the existing prototypes of 4 rotor-craft don't analyze the propeller, motor characteristic and propose a methodology to optimize this system. In design of propeller, experimental results show that thrust and power are relatively efficient at a pitch angel of 20 degree. To the conclusion, the design method and optimization method of the propeller, motor, frame, Blimp, which are the main design elements of the blimp type 4 rotor craft, were studied to optimize the existing Blimp 4 rotor craft body design method.
목차
1. 서론
2. Blimp형 4 날개 회전 비행체의 비행 원리
3. Blimp 4 날개 회전 비행체의 설계
3.1 날개설계를 위한 공중정지 이론
3.2 모터 선정(motor selection)
3.3 프로펠러 설계
3.4 Blimp 설계
3.5 프레임
3.6 Blimp type 4 날개 회전 비행체 설계
4. 결론
References