FIELD: physics; measurement.
SUBSTANCE: invention relates to instrument making and can be used for determining the width of a corridor for safe aircraft manoeuvring. To achieve technical outcome, the device contains: a device (3), which can be used by an operator to input several errors, each of which affects automatic flight of the aircraft at low altitude; device (4) for determining probability of exit from the corridor, where such an exit is not allowed; and a device (5) for determining the width of the said corridor for safe manoeuvring based on the above mentioned errors and probability of exit, based on at least one mathematical expression which links at least, the error, probability of exit and the width.
EFFECT: more functional capabilities.
17 cl, 3 dwg
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