FIELD: transport.
SUBSTANCE: set of inventions relates to aviation. Device for aerodynamic coefficient estimation contains device (5) for deflection angle command signal generation. Device (6) for registration of control surface motion parameter based on deflection angle command signal, calculation device (7) and device (8) for determination of aerodynamic coefficient estimated value. Device for detection of failure/damage of control surface contains estimation device and device for aerodynamic coefficient estimation.
EFFECT: set of inventions is aimed to detect control surface failure/damage while decreasing discomfort for passengers.
8 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT CONTROL SYSTEM, AIRCRAFT CONTROL METHOD AND AIRCRAFT | 2011 |
|
RU2537883C2 |
| AEROPLANE CONTROL SYSTEM, AEROPLANE AND AEROPLANE CONTROL METHOD | 2012 |
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|
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|
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| AUTOMATIC UNMANNED DIAGNOSTIC COMPLEX | 2011 |
|
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| METHOD AND DEVICE FOR PROTECTION OF MAXIMUM LIFT OF AN AIRCRAFT | 2016 |
|
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| SYSTEM AND METHOD FOR DETECTING ERRONEOUS PRESSURE MEASUREMENTS IN AIR SIGNAL SYSTEM WITH NON-PROTRUDING PRESSURE RECEIVERS USING PRESSURE DIAGRAMS BETWEEN ADJACENT PRESSURE SAMPLING HOLES | 2019 |
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RU2771090C1 |
