• Title/Summary/Keyword: MPUH

Search Result 2, Processing Time 0.015 seconds

Design and Implementation of Control Program for EO/IR Camera mounted on Multi-Purpose Unmanned Helicopter

  • Ahn, MyeongGi;Seong, KilYoung;Lee, JongHun;Kim, JaeKyung
    • Journal of Aerospace System Engineering
    • /
    • v.15 no.6
    • /
    • pp.72-77
    • /
    • 2021
  • This paper proposes a design and development plan for a control program for the MX-10 EO/IR camera. This camera is a piece of mission equipment mounted on the multi-purpose unmanned helicopter (MPUH) system. Operators must be able to control the necessary functions of the camera to perform their assigned tasks. To achieve this, the function to control the camera was analyzed, and a control program was developed. In addition, the control program was linked to a joystick for convenient operation of the camera by the operator.

Cross-sectional Design and Stiffness Measurements of Composite Rotor Blade for Multipurpose Unmanned Helicopter (다목적 무인헬기 복합재 로터 블레이드의 단면 구조설계 및 강성 측정)

  • Kee, Young-Jung;Kim, Deog-Kwan;Shin, Jin-Wook
    • Journal of Aerospace System Engineering
    • /
    • v.13 no.6
    • /
    • pp.52-59
    • /
    • 2019
  • The rotor blade is a key component that generates the lift, thrust, and control forces required for helicopter flight by the torque transmitted through the hub and the blade pitch angle control, and should be designed to factor vibration characteristics so that there is no risk of resonance with structural safety. In this study, the structural design of the main rotor blade for MPUH(Multi-Purpose Unmanned Helicopter) was conducted and the sectional stiffness measurement of the fabricated blade was performed. The evaluation of the vibration characteristics of the main rotor system was then conducted factoring the measured stiffness distribution. The interior of the rotor blade comprised of the skin, spar, and torsion box, and carbon and glass fiber composites were applied. The Ksec2D program was applied to predict the stiffness of blade, and the results were compared to the measured data. CAMRADII, a comprehensive rotorcraft analysis program, was applied to investigate the natural frequency trends and resonance risks due to the rotor rotation.