FIELD: automatic control systems.
SUBSTANCE: automatic control system for the roll and heading of an unmanned aerial vehicle (UAV) during landing comprises an aileron control drive, a rudder control drive, a crosswind identifier, a driver of setting actions, an adaptive setting action switch, a gear ratio switch, an adaptive aileron control controller, an adaptive control controller rudder, connected in a certain way.
EFFECT: invention ensures the safety of the landing in the presence of strong winds.
1 cl, 19 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
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|
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| AIRCRAFT LATERAL MOVEMENT AUTOMATED MODAL CONTROL SYSTEM | 2015 |
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| METHOD FOR AUTOMATIC CONTROL OF LONGITUDINAL MOVEMENT OF AIRCRAFT LANDING | 2015 |
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RU2588173C1 |
