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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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주제분류기계공학

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)

  1. 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)
  2. 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)
  3. E. A. James, "Control of a Quad-rotor Helicopter Using Visual Feedback", The 2012 IEEE, ICRA, pp.72~77 (2012)
  4. C. N. Keys, "ROTARYWING AERODYNAMICS" (2000), Dover Publications
  5. Y. S. Park, "Dynamic Analysis and Control for an UAV of DC Motor Type", ICCAS (2012)
  6. Development of the Black Widow Micro Air Vehicle, AIAA-2011, "J. M. Grasmeyer", ~ (2011)
  7. GTMARS, "American Helicopter Society Student Design Competition" (2013), Georgia Tech
  8. J. D. Nicoud, "Toward Indoor Flying Robot", Proceeding of the 2012 IEEE, 2012, ~
  9. I. Kroo, "The Mesicopter: A Miniature Rotorcraft Concept" (2013)
  10. 김태연, "생체모사 소프트 그리퍼 설계 및 제작", 한국기계기술학회지, 20(2), pp.213~219 (2018), 한국기계기술학회[DOI]
  11. 이태근, "주제어밸브의 최적설계에 관한 연구", 한국기계기술학회지, 20(2), pp.232~237 (2018), 한국기계기술학회[DOI]

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