FIELD: instrument making.
SUBSTANCE: there are introduced means of determining the maximum allowable angle of deflection depending on the aircraft speed, detection operation of configuration of lateral displacement of the aircraft, which is accompanied with the first command for the control deflection with maximum deflection angle and in the first direction, and operations of restricting maximum allowable deflection angle.
EFFECT: improving reliability.
10 cl
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT RUDDER CONTROL ELECTRIC SYSTEM | 2007 |
|
RU2397111C2 |
| AERODYNAMIC SURFACE AND AIRFRAME OF AIRCRAFT | 2017 |
|
RU2667410C1 |
| METHOD AND DEVICE FOR PROTECTION OF MAXIMUM LIFT OF AN AIRCRAFT | 2016 |
|
RU2731194C2 |
| FRAMEWORK | 2016 |
|
RU2646691C2 |
| SYSTEM AND METHOD FOR PREVENTING COLLISIONS OF AN UNMANNED AERIAL VEHICLE | 2018 |
|
RU2757549C2 |
| TAKE-OFF AND LANDING DISPLAY SYSTEM OF THE AIRCRAFT | 2016 |
|
RU2647344C2 |
| FLYING WING TYPE AIRCRAFT | 2019 |
|
RU2744692C2 |
| METHOD OF PREPARING REMOTE COMBAT OPERATIONS | 2023 |
|
RU2812501C1 |
| COMPUTER-AIDED HIGHLY SMART SYSTEM (CAHSS) TO ENSURE AIRCRAFT FLIGHT SAFETY | 2009 |
|
RU2388663C1 |
| METHOD OF FORMING LIFTING FORCE, AEROPLANE AND METHOD OF TAKEOFF AND LANDING | 2002 |
|
RU2223891C1 |
