FIELD: aviation.
SUBSTANCE: adaptive system with reference model for control of aircraft, containing two adders, three multiplying units, three integrators, a correcting element, a comparison unit, a self-adjustment algorithms unit, the reference model, angle sensors, angular velocity and linear acceleration sensors, steering actuator connected in a certain manner.
EFFECT: extension of functionality of the control system of the aircraft due to introduction of the adaptation circuit to the change of the aerodynamic damping, improved quality of flight at change of flight conditions.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SYSTEM FOR PREDICTION OF FUEL-SCALE TEST RESULTS OF UNMANNED AIRCRAFT | 2000 |
|
RU2163732C1 |
| SYSTEM FOR PREDICTING RESULTS OF NATURE TESTING OF DRONE AIRCRAFT | 1999 |
|
RU2163387C1 |
| FLYING VEHICLE AUTOMATIC LANDING SYSTEM | 2004 |
|
RU2284058C2 |
| REMOTE REDUNDANT SYSTEM OF AUTOMATED MODAL CONTROL IN LONGITUDINAL CHANNEL OF MANEUVERED MANNED AND UNMANNED AIRCRAFTS | 2015 |
|
RU2645589C2 |
| SYSTEM FOR PREDICTING UNMANNED AIRCRAFT FULL-SCALE TEST RESULTS | 2000 |
|
RU2160927C1 |
| SIMULATOR COMPLEX FOR CHECKING CONTROL SYSTEM OF UNMANNED AIRCRAFT | 2010 |
|
RU2432592C1 |
| ADAPTIVE SYSTEM FOR CONTROLLING A MANNED AERIAL VEHICLE IN THE ROLL CHANNEL | 2020 |
|
RU2753776C1 |
| ADAPTIVE BANK ANGLE AUTO-PILOT | 2004 |
|
RU2272747C2 |
| AIRCRAFT LATERAL MOVEMENT AUTOMATED MODAL CONTROL SYSTEM | 2015 |
|
RU2618652C1 |
| METHOD OF CONTROL OF ANGULAR MOTION OF AIRCRAFT WITH INTEGRATING DRIVE | 2007 |
|
RU2335005C1 |
