Control Optimization in Aerospace Engineering at Stochastic Perturbations and Stream of Faults

Abstract

The necessary optimality conditions are studied for stochastic controlled systems with random abrupt nature to describe the operation of a flying vehicle with various requirements due to disturbances, random parameters spread, additive and multiplicative noises, and also random Poisson stream of the system failures. We research the problem on the spacecraft inter-orbital flight at failures of the working jet engines.