FIELD: physics; transport.
SUBSTANCE: director includes a display and processor unit with function of graphic display generation on the display in the form of a concave pitch scale with a mean vertical. At that, the invention implements functional connection of spatial graphic model change by the aircraft according to the digital signals corresponding to precession of separate electric gyroscopes.
EFFECT: extension of functional capabilities.
9 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR INTEGRAL DISPLAY OF FLIGHT SITUATION PARAMETERS | 2019 |
|
RU2722888C1 |
FLIGHT DIRECTOR DISPLAY | 2011 |
|
RU2474862C1 |
METHOD OF FORMING PILOTAGE NAVIGATION INFORMATION ON MULTI-FUNCTIONAL INDICATOR FOR PERFORMING LANDING | 2005 |
|
RU2297596C1 |
ELECTRONIC ARTIFICIAL HORIZON | 2017 |
|
RU2664789C1 |
TAKE-OFF AND LANDING DISPLAY SYSTEM OF THE AIRCRAFT | 2016 |
|
RU2647344C2 |
FLIGHT DIRECTOR | 2002 |
|
RU2207514C1 |
DEVICE FOR PERIPHERAL INDICATION OF LOCATION AND MOVEMENT OF HORIZON LINE IN FLIGHT | 2006 |
|
RU2315957C1 |
HELICOPTER FLIGHT COMMAND INDICATOR | 2013 |
|
RU2539708C1 |
COMMAND AND FLIGHT INDICATOR OF HELICOPTER | 2020 |
|
RU2778716C2 |
FLIGHT DIRECTOR DISPLAY | 2018 |
|
RU2711196C1 |
Authors
Dates
2008-08-20—Published
2006-10-06—Filed