Application of stochastic optimal control to the suboptimal design of thrust-mass profiles |
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Authors: | Y. Yavin |
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Affiliation: | (1) Department of Electrical and Electronic Engineering, University of Pretoria, Pretoria, South Africa |
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Abstract: | Stochastic optimal control techniques are applied to compare the performance of identical medium-range air-to-air missiles which have different thrust-mass profiles. The measure of the performance is the probability of reaching a lock-on-point with a favorable range of guidance and flight parameters, during a fixed time interval [0,tf], given that, during the flight, the trajectories of the missile are subjected to a variety of constraints including dynamic pressure constraints. |
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Keywords: | Stochastic optimal control thrust-mass profiles dynamic pressure constraints |
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