FIELD: aircraft engineering.
SUBSTANCE: proposed method consists in generation of control signal input into stabilisation unit by its calculation on differential game basis. Said control signal is calculated proceeding from analysis of location of minimax region drone attainability domain constructed with due allowance for all possible disturbances satisfying preset constraints and preset normal overload magnitude.
EFFECT: control signal with compensated constrained disturbances with unknown statistical properties.
5 dwg
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