피치각에 따른 Blimp형 Rotor Craft Blade의 설계에 관한 연구
A Study on the Design of Blimp Type Rotor Craft Blade according to Pitch Angle
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초록
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.
Abstract
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.
참고문헌 (11)
- M. Saeki, "Flight control design and experiment of a twin rotor helicopter model via 2 step exact linearization", Proc. IEEE Int. Conf. on control Application, pp.146~151 (2010)
- V. Mistler, "Exact linearization and non-interacting control of a 4 rotors helicopter via dynamics feedback", IEEE International Workshop on Robot and Human Interactive Communication, pp.586~593 (2011)
- E. A. James, "Control of a Quad-rotor Helicopter Using Visual Feedback", The 2012 IEEE, ICRA, pp.72~77 (2012)
- C. N. Keys, "ROTARYWING AERODYNAMICS" (2000), Dover Publications
- Y. S. Park, "Dynamic Analysis and Control for an UAV of DC Motor Type", ICCAS (2012)
- Development of the Black Widow Micro Air Vehicle, AIAA-2011, "J. M. Grasmeyer", ~ (2011)
- GTMARS, "American Helicopter Society Student Design Competition" (2013), Georgia Tech
- J. D. Nicoud, "Toward Indoor Flying Robot", Proceeding of the 2012 IEEE, 2012, ~
- I. Kroo, "The Mesicopter: A Miniature Rotorcraft Concept" (2013)
- 김태연, "생체모사 소프트 그리퍼 설계 및 제작", 한국기계기술학회지, 20(2), pp.213~219 (2018), 한국기계기술학회[DOI]
- 이태근, "주제어밸브의 최적설계에 관한 연구", 한국기계기술학회지, 20(2), pp.232~237 (2018), 한국기계기술학회[DOI]
