FIELD: aviation technology.
SUBSTANCE: invention relates to the field of aviation technology, it is designed for the use in educational and research purposes. The flight stand of a maneuverable aircraft with an electromechanical limiter of limit modes contains a sequentially connected unit of command control levers, a unit of position sensors of command control levers, a unit of spatial aircraft movement, a unit of visualization of spatial aircraft movement, a system of visualization of spatial aircraft movement, a sequentially connected unit of setting initial conditions, a unit of dynamics of the power plant, interacting with the unit of spatial aircraft movement. The stand also contains a sequentially connected unit of limit mode limiter and a unit of shaking simulation for the control handle and mechanical stop. The fourth output of the unit of spatial aircraft movement is connected to the input of the unit of limit mode limiter, and the output of the unit of shaking simulation for the control handle and mechanical stop is connected to the input of the unit of command control levers.
EFFECT: accuracy of the results obtained in the study of the dynamics of the aircraft flight in near-critical and critical flight modes is increased.
1 cl, 1 dwg
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Authors
Dates
2021-08-11—Published
2020-10-29—Filed