FIELD: aviation.
SUBSTANCE: group of inventions relates to a system and method of controlling one or more flaps of an aircraft. Control system comprises two flaps configured to move towards aircraft wing, two drives connected to flap, two sensors, determining position or speed of drives, control unit. To control flaps of aircraft receive signals from position sensors or speed of drives, signals of the first and second sensors are compared, the speed of one or both sensors is adjusted based on the difference of signals.
EFFECT: preventing or minimizing flaps or twisting of flaps during operation.
20 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT CONTROL SYSTEM | 2017 |
|
RU2737766C2 |
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|
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|
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|
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AIRCRAFT | 2008 |
|
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|
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AIRCRAFT CONTROL METHOD, CONTROL SYSTEM AND AIRCRAFT | 2017 |
|
RU2688559C2 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH HYBRID POWER PLANT | 2017 |
|
RU2724940C2 |
Authors
Dates
2020-07-28—Published
2017-02-20—Filed