FIELD: unmanned aerial vehicles.
SUBSTANCE: invention relates to a method for automatic control of the longitudinal movement of the UAV in the presence of wind disturbances. To do this, a control signal is formed, during the formation of which a signal is used to estimate the increment in the angle of attack caused by wind disturbance, passed through the isodromic link and multiplied by the transfer coefficient, and a discrete optimal Kalman filter is also formed. Next, the generated control signal is fed to the input of the elevator drive.
EFFECT: increased flight safety in the presence of wind disturbances.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AUTOMATIC STABILITY DEVICE OF UNMANNED SMALL-SIZED VEHICLE | 1988 |
|
SU1826781A1 |
| DEVICE FOR CONTROLLING SIDEWARD MOVEMENT OF AN AIRCRAFT | 2005 |
|
RU2289839C1 |
| DEVICE FOR CONTROLLING SIDE MOVEMENT OF AN AIRCRAFT | 2004 |
|
RU2262730C1 |
| AIRCRAFT LATERAL MOVEMENT AUTOMATED MODAL CONTROL SYSTEM | 2015 |
|
RU2618652C1 |
| DEVICE FOR COORDINATED REGULATION OF ANGULAR LATERAL MOVEMENT OF FLYING VEHICLE | 1990 |
|
RU2047888C1 |
| AIRCRAFT APPROACH LANDING ACS | 2006 |
|
RU2330792C1 |
| AUTOMATIC CONTROL SYSTEM FOR THE ROLL AND HEADING OF AN UNMANNED AERIAL VEHICLE DURING LANDING | 2022 |
|
RU2784883C1 |
| AIRCRAFT CONTROL SYSTEM | 2011 |
|
RU2482022C1 |
| METHOD FOR CONTROLLING SIDEWARD MOVEMENT OF AN AIRCRAFT | 2005 |
|
RU2289838C1 |
| METHOD FOR AUTOMATIC CONTROL OF AIRCRAFT AT LANDING AND SYSTEM THEREFOR | 2014 |
|
RU2581215C1 |
