FIELD: aviation.
SUBSTANCE: group of inventions relates to a system and method for compensation of an air mass burst, an airborne aircraft. System comprises a sensor subsystem, an air mass burst signal subsystem configured to output a signal for movement of control surfaces in response to said signal. Method includes detecting at least one parameter of an airborne aircraft using a first sensor arranged near a front portion of an aircraft, outputting a first signal based on said at least one parameter from first sensor, detecting said at least one airborne vehicle parameter by second sensor, outputting a second signal based on said at least one parameter from the second sensor, using the air bursting signal subsystem to generate an airflow burst signal based on analyzing the first and second signals, change of signal of load parameter with the help of burst signal of air mass in response to signal of air mass burst. Aircraft comprises air mass flow compensation system configured to adaptively reduce load as a result of air mass burst affecting airborne aircraft.
EFFECT: providing adaptive load reduction as a result of air mass impact acting on aircraft.
20 cl, 5 dwg
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Authors
Dates
2019-11-19—Published
2016-03-02—Filed