FIELD: controlling.
SUBSTANCE: sideslip prevention system installed on a manned aerial vehicle comprises a control post with control bodies made, in particular, in the form of control pedals providing control of the aerial vehicle in the yaw channel, comprises activation means including at least one electronic control unit, at least one input signal source, and two vibrators, wherein each vibrator is structurally connected with one of the control pedals and configured to transmit vibration to one of the feet of the pilot when the threshold value of the lateral overload component or the sideslip angle is exceeded.
EFFECT: prevention of sideslip of an aerial vehicle.
10 cl, 11 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STALLING WARNING SYSTEM | 2017 |
|
RU2653414C1 |
| PILOT SEAT | 2016 |
|
RU2610325C1 |
| AIRCRAFT WARNING SYSTEM | 2017 |
|
RU2653417C1 |
| AIRCRAFT | 2016 |
|
RU2624760C1 |
| FRAMEWORK | 2016 |
|
RU2646691C2 |
| AIRCRAFT CONTROL SYSTEM | 2016 |
|
RU2630567C1 |
| AERODYNAMIC SURFACE AND AIRFRAME OF AIRCRAFT | 2017 |
|
RU2667410C1 |
| WING WITH AERODYNAMIC CURTAIN | 2016 |
|
RU2646686C2 |
| ACCELERATOR ASSEMBLY OF INTERNAL COMBUSTION ENGINE WITH TURBO-SUPERCHARGE | 2018 |
|
RU2681805C1 |
| TRACTION CONTROL SYSTEM | 2017 |
|
RU2688081C1 |
