Journal of the Korean Society for Aviation and Aeronautics (한국항공운항학회지)

The Korean Society for Aviation and Aeronautics (한국항공운항학회)
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Derivation and Verification of the Relative Dynamics Equations for Aerial Refueling

공중재급유를 위한 상대운동방정식 유도 및 검증

  • 장지은 (과학기술연합대학원대학교 한국항공우주연구원) ;
  • 이상종 (한국항공우주연구원 항공제어전자팀) ;
  • 유혁 (한국항공우주연구원 항공제어전자팀)
  • Received : 2013.09.23
  • Accepted : 2013.12.18
  • Published : 2013.12.31
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Abstract

This paper addresses the derivation of 6-DOF equation of Tanker and Receiver's aircraft for aerial refueling. The new set of nonlinear equations are derived in terms of the relative translational and rotational motion of receiver aircraft respect to the tanker aircraft body frame. Further the wind effect terms due to the tanker's turbulence are included. The derivation of absolute dynamic equation for tanker aircraft written in the inertial frame is calculated from the relative dynamics equations of receiver. The derived relative and absolute equations are implemented the simulation in the same flight conditions to verify the relative motion and compare the trim results by using the MATLAB/SIMULINK program.

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References

  1. Mao, W., Eke, F.O., "A survey of the Dynamics and Control of Aircraft During Aerial Refueling", Nonlinear Dynamics and System Theory, 2008
  2. Nalepka, J., Hinchman, J., "Automated Aerial Refueling: Extending the Effectiveness of Unmanned Air Vehicles", AIAA Modeling and Simulation Technologies Conference and Exhibit, California, Aug 2005
  3. Waishek, J., "Derivation of the dynamics equations for receiver aircraft in aerial refueling", M.S thesis, The University of Texas at Arlington, Arlington, Dec 2007
  4. Kim, E., Dogan, A., Blake, W., "Control of a Receiver Aircraft Relative to the Tanker in Racetrack Maneuver", AIAA Guidance Navigation and Control Conference and Exhibit, Keystone, Colorado, Aug 2006
  5. Venkataramanan, S., Dogan, A., "Dynamic Effects of Trailing Vortex with Turbulence & Time-varying Inertia in Aerial Refueling", AIAA Atmospheric Flight Mechanics Conference and Exhibit, Rhode Island, Aug 2004
  6. Tucker, J., Dogan, A., "Derivation of the Dynamics Equations of Receiver Aircraft in Aerial Refueling", AIAA Aerospace Science Meeting and Exhibit, Reno, Nevada, Jan 2007
  7. Dogan, A., Sato, S., "Flight Control and Simulation for Aerial Refueling", AIAA Guidance Navigation and Control Conference and Exhibit, San Francisco, California, Aug 2005

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