On Optimizing Control in Aerospace Engineering at Perturbations, Restrictions and Stream of Faults

TL;DRAbstract

Abstract: This paper presents the study of necessary optimum control conditions for stochastic systems of random abrupt nature to describe the operation of a flying vehicle being bounded by various system objectives and requirements, and being subjected to disturbances conditioned by random parameters spread, additive and multiplicative noise, and random Poisson stream of subsystem failures. The inter-orbit flight problem being subject to a failure of one of two sections of simultaneously working engines is analyzed.

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