We address, using probabilistic modeling and the extreme-value-distribution technique, the helicopter undercarriage strength in a helicopter-landing-ship situation. Our analysis contains an attempt to quantify, on the probabilistic basis, the role of the human factor in the situation in question. This factor is important from the standpoint of the operation time that affects the likelihood of safe landing during the lull period in the sea condition. The operation time includes (1) the time required for the officer-on-ship-board and the helicopter pilot to make their go-ahead decisions and (2) the time of actual landing. It is assumed, for the sake of simplicity, that both these times could be approximated by Rayleigh’s law, while the lull duration follows the normal law with a high enough ratio of the mean value to the standard deviation. Safe landing could be expected if the probability that it occurs during the lull time is sufficiently high. The probability that the helicopter undercarriage strength is not compromised can be evaluated as a product of the probability that landing indeed occurs during the lull time and the probability that the relative velocity of the helicopter undercarriage with respect to the ship’s deck at the moment of encounter does not exceed the allowable level. This level is supposed to be determined for the helicopter-landing-ground situation. The developed model can be used when developing specifications for the undercarriage strength, as well as guidelines for personnel training. Particularly, the model can be of help when establishing the times to be met by the two humans involved to make their go-ahead decisions for landing and to actually land the helicopter. Plenty of additional risk analyses (associated with the need to quantify various underlying uncertainties) and human psychology related efforts will be needed, of course, to make such guidelines practical.
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February 2010
Safety And Reliability
Helicopter Landing Ship: Undercarriage Strength and the Role of the Human Factor
E. Suhir
e-mail: suhire@aol.com
E. Suhir
Bell Laboratories
, Physical Sciences and Engineering Research Division, Murray Hill, NJ 07974; Department of Electrical Engineering, University of California
, Santa Cruz, CA 95064; Department of Mechanical Engineering, University of Maryland
, College Park, MD 20742; ERS Company
, Los Altos, CA 94024
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E. Suhir
Bell Laboratories
, Physical Sciences and Engineering Research Division, Murray Hill, NJ 07974; Department of Electrical Engineering, University of California
, Santa Cruz, CA 95064; Department of Mechanical Engineering, University of Maryland
, College Park, MD 20742; ERS Company
, Los Altos, CA 94024e-mail: suhire@aol.com
J. Offshore Mech. Arct. Eng. Feb 2010, 132(1): 011603 (6 pages)
Published Online: December 22, 2009
Article history
Received:
September 19, 2008
Revised:
August 17, 2009
Online:
December 22, 2009
Published:
December 22, 2009
Citation
Suhir, E. (December 22, 2009). "Helicopter Landing Ship: Undercarriage Strength and the Role of the Human Factor." ASME. J. Offshore Mech. Arct. Eng. February 2010; 132(1): 011603. https://doi.org/10.1115/1.4000497
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