FIELD: instrument making.
SUBSTANCE: invention provides for mobility of a launching setup of an unmanned aircraft relative to a control station at which it is installed, possible control of the unmanned aircraft in a narrow-band optic information control field considering external conditions, available interference and mobility of the control station. The invention provides for possible correction of control commands to create additional unmanned aircraft manoeuvrability capabilities relative to the specified direction. Maximum level of corrected control commands of the unmanned aircraft is restricted with limits of its allowable transverse accelerations, and a deviation value from the specified direction is restricted with sizes of the information control field.
EFFECT: improving control efficiency by independent introduction of additional corrections to each of guidance drives of the unmanned aircraft and improving guidance accuracy.
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Authors
Dates
2014-01-20—Published
2012-09-06—Filed