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잠수함의 종동요각 한계예측 알고리즘 설계

Design of Pitch Limit Detection Algorithm for Submarine

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참고문헌

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주제분류해양공학

초록

An envelope protection system is a control system that allows a submarine to operate freely using its own operational envelope without exceeding the structural limit, dynamic limit, and control input limit. In this paper, an envelope protection system for the pitch angle of a submarine is designed using a dynamic trim algorithm. A linear quadratic regulator and artificial neural network are used for the true dynamics approximation. A submarine maneuvering simulation program developed using experimental data is used to validate the designed envelope protection system. Simulation results show the effectiveness of the designed envelope protection system.

Abstract

An envelope protection system is a control system that allows a submarine to operate freely using its own operational envelope without exceeding the structural limit, dynamic limit, and control input limit. In this paper, an envelope protection system for the pitch angle of a submarine is designed using a dynamic trim algorithm. A linear quadratic regulator and artificial neural network are used for the true dynamics approximation. A submarine maneuvering simulation program developed using experimental data is used to validate the designed envelope protection system. Simulation results show the effectiveness of the designed envelope protection system.

참고문헌 (17)

  1. Bateman, A. J, "Piloted Simulation Evaluation of a Neural Network Limit Avoidance System for Rotorcraft", 24th Atmospheric Flight Mechanics Conference, pp.4252~ (1998)
  2. Burcher, R, "Concepts in Submarine Design(2)" (1995), Cambridge University Press
  3. Falkena, W, "Investigation of Practical Flight Envelope Protection Systems for Small Aircraft", Journal of Guidance, Control, and Dynamics, 34(4), pp.976~988 (2011)
  4. Standard Equations of Motion for Submarine Simulation, "Gertler, M", NSRDC, ~, pp.Report 2510 (1967)
  5. Gursoy, G, "Engine Limit Detection and Avoidance for Helicopters with Multiple Limits", AIAA Atmospheric Flight Mechanics Conference (2013)
  6. Gursoy, G, "Non-Iterative Adaptive Limit and Control Margin Estimation with Concurrent Learning", Proceedings of AIAA Atmospheric Flight Mechanics Conference, SciTech 2015, Kissemmee, FL (2015)
  7. Horn, J.F, "Flight Envelope Limiting Systems using Neural Networks", Proceedings of the AIAA Atmospheric Flight Mechanics Conference, pp.741~751 (1998)
  8. Horn, J, "Flight Envelope Limit Detection and Avoidance for Rotorcraft", Journal of the American Helicopter Society, 47(4), pp.253~262 (2002)
  9. Horn, J. F, "Detection and Avoidance of Main Rotor Hub Moment Limits on Rotorcraft", Journal of Aircraft, 41(2), pp.372~379 (2004)
  10. Sahani, N.A, "Envelope Protection Systems for Piloted and Unmanned Rotorcraft", Doctor, pp.2005
  11. 신호현, "항공기의 수평속도에 대한 비행영역 보호 시스템 설계", 한국항공우주학회지, 38(4), pp.327~334 (2010), 한국항공우주학회
  12. 신효현, "Design of a Flight Envelope Protection System Using a Dynamic Trim Algorithm", International Journal of Aeronautical and Space Sciences, 12(3), pp.241~251 (2011), 한국항공우주학회
  13. 박종용, "적응제어기법을 이용한 수면근처에서 운항하는 몰수체의 심도제어기 설계", 한국해양공학회지, 29(3), pp.270~282 (2015), 한국해양공학회
  14. Unnikrishnan, S, "Adaptive Dynamic Trim Prediction for Limit Detection and Avoidance", AIAA Atmospheric Flight Mechanics Conference (2003)
  15. Yavrucuk, I, "Carefree Maneuvering Using Adaptive Neural Networks", Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit (2002)
  16. Yavrucuk, I, "Adaptive Limit Margin Detection and Limit Avoidance", Doctor, pp.2003
  17. Yavrucuk, I, "Envelope Protection for Autonomous Unmanned Aerial Vehicles", Journal of Guidance, Control, and Dynamics, 32(1), pp.248~261 (2009)

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