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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
1

A system dynamics approach to aircraft survivability-attrition analysis

Santoso, Iwan B. January 1984 (has links)
Mathematical representation of military operations have long fascinated analysts and practitioners. In 1916 English mathematician Frederick W. Lanchester represented the attrition rates of two opposing forces in the form of two differential equations, functions of the size and combat effectiveness of each side. Lanchester's model was an intellectual breakthrough in the analysis of warfare insofar as it provided a deep insight into the possibilities inherent in simple models of combat. Interestingly enough, Lanchester's representation of the problem as a dynamic system is precisely the approach used in the system dynamics methodology employed here. In system dynamics, differential equations are converted to difference equations and there is virtually no limit to the number that can be employed to represent the known and complex details of a system. The attrition model developed here describes the interaction between twelve types of U.S. combat aircraft and twelve types of U.S.S.R. combat aircraft and indicates the winner or the loser at the end of an engagement or a battle during wartime. To guide the peacetime preparations, a generic baseline and modified aircraft are utilized and compared using an adaptation of the attrition model, so as to decide if the proposed modification of U.S. aircraft should be undertaken or not. Two measures of effectiveness are presented to evaluate the overall performance of the modified aircraft compared to the baseline aircraft -- decreased program life cycle cost and increased payload delivered to target per aircraft lost. Scenario analyses are performed to assess the combat aircraft effectiveness under changes to endogenous and exogenous parameters. / Ph. D.
2

Considerations in the development of a survivability/lethality tradeoff submodel for advanced tactical aircraft conceptual design

Kadari, Venugopal Rao January 1985 (has links)
System dynamics is based on principles borrowed from engineering—especially feedback concepts. It makes possible a representation of decision policies and information flow. The systems approach is a mixture of scientific approaches to conceptualizing problems and solving them through research, design and analysis. In system dynamics, differential equations are represented in the form of difference equations. There is no limit to the number that can be employed to represent the complex details of any system. The models developed here help in determining the superiority or inferiority of the Advanced Tactical Aircraft (ATA) over the baseline aircraft. The advanced tactical aircraft is a proposed replacement aircraft that can undertake any of the three missions—air superiority, fleet defense and attack/interdiction. The baseline aircraft for air superiority and fleet defense is the Tomcat Fighter, F-14 and for attack/interdiction it is Intruder, A-6. Several measures of effectiveness are presented to evaluate the superiority or inferiority of the replacement aircraft over the baseline aircraft. / Master of Science / incomplete_metadata

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