FIELD: aircraft engineering.
SUBSTANCE: proposed method comprises determining current control parametre, comparing the latter with preset reference value, determining current level of aircraft control stick deviation, and comparing the latter with present deviation angle. If control parametres exceeds preset value and current deviation angle exceeds preset value, visual alarm signal is displayed. Proposed device comprises first device to determine current control parametre, second device to compare current parametre with preset values, third device to determine current deviation of aircraft control stick and fourth device to compare the latter with preset value. It comprises also fifth device representing an operating data display.
EFFECT: warning on oncoming aircraft critical control state.
13 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD AND SYSTEM FOR DEVIATION FROM COLLISIONS FOR AIRCRAFT | 2005 |
|
RU2343528C1 |
| FLIGHT DIRECTOR | 2002 |
|
RU2207514C1 |
| FLIGHT DIRECTOR DISPLAY | 2011 |
|
RU2474862C1 |
| STALLING WARNING SYSTEM | 2017 |
|
RU2653414C1 |
| METHOD FOR INTEGRAL DISPLAY OF FLIGHT SITUATION PARAMETERS | 2019 |
|
RU2722888C1 |
| METHOD AND SYSTEM FOR ASSISTING FLYING AIRCRAFT AT LOW ALTITUDE | 2006 |
|
RU2388058C2 |
| METHOD AND DEVICE TO FACILITATE AIRCRAFT LANDING | 2007 |
|
RU2389659C1 |
| COMMAND AND FLIGHT INDICATOR OF HELICOPTER | 2020 |
|
RU2778716C2 |
| METHOD AND DEVICE FOR PILOTING OF AIRCRAFT AND AIRCRAFT | 2002 |
|
RU2241642C2 |
| ELECTRONIC ARTIFICIAL HORIZON | 2017 |
|
RU2664789C1 |
