A target missile engagement scenario using classical proportional navigation

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Author
Lukenbill, Francis C.
Date
1990-12Advisor
Titus, Harold A.
Second Reader
Powell, James R.
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This thesis deals with a simulation of a missile versus target engagement scenario. After driving simplified transfer functions for the missile seeker head, missile autopilot, missile dynamics, and target dynamics, a three dimensional simulation is developed using classical proportional navigation. The scenario is simulated using state variable design. A forward time solution of the two dimensional problem is developed which is converted to an adjoint model. The adjoint model is used to determine the optimal time to initiate simplified and tactical evasion maneuvers in order to maximize the final miss distance.
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This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.Collections
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