FIELD: aviation.
SUBSTANCE: each flying control contains: a control knob (21, 31), the force sensor (24, 34), designed to provide the force value (Fp, Fcp) of piloting, provided by the pilot, and the correction device. The correction device consists a comparator (11), a corrector with a deadspot (12) and an adder unit (14) for generating a force value feedback.
EFFECT: improved performance.
12 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD AND DEVICE FOR INTERRELATION BETWEEN PILOTING BODIES, PILOTING UNIT AND AIRCRAFT | 2016 |
|
RU2693516C2 |
| METHOD OF CONTROLLING OPERATION OF AIRCRAFT PILOTING DEVICE AND AIRCRAFT PILOTING DEVICE | 2014 |
|
RU2671442C2 |
| METHOD TO CONTROL AERODYNAMIC MEANS OF FLYING VEHICLE, CORRESPONDING CONTROL SYSTEM AND FLYING VEHICLE EQUIPPED WITH SUCH CONTROL SYSTEM | 2016 |
|
RU2643300C2 |
| METHOD AND DEVICE TO FLY AIRCRAFT RELATIVE TO ONE PILOTAGE AXIS | 2006 |
|
RU2381958C2 |
| FLYING VEHICLE | 1997 |
|
RU2148528C1 |
| AIRCRAFT ELECTRONIC CONTROL COMPONENT FOR AIRCRAFT CONTROL UNIT, AIRCRAFT CONTROL UNIT AND AIRCRAFT WITH SAID CONTROL DEVICE | 2010 |
|
RU2537364C2 |
| AIRCRAFT SIDE-STICK CONTROL | 2014 |
|
RU2571992C1 |
| SIDESLIP PREVENTION SYSTEM | 2020 |
|
RU2759370C1 |
| COMMAND CENTRE FOR MANUAL CONTROL OF AIRCRAFT | 2020 |
|
RU2751721C1 |
| CONTROL OVER HYBRID HELICOPTER SPEED | 2012 |
|
RU2525357C2 |
