FIELD: aviation.
SUBSTANCE: system of automatic control of the angle of inclination and limitation of the heel angle of the aircraft contains a heading angle adjuster, four comparison elements, calculator of a given roll angle, algebraic selector of the minimum signal, computer autopilot roll angle, aileron servo, course angle sensor of the aircraft, roll angle sensor of the aircraft, setting device of the maximum angle of heel, setting device of the minimum angle of heel, the third element of comparison, algebraic selector maximum signal, connected in a certain way.
EFFECT: required accuracy of limiting the angle of heel when the aircraft turns to a given course angle is provided.
1 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT BANK ANGLE BANK AND ANGULAR SPEED LIMITING AUTOMATIC CONTROL SYSTEM | 2012 |
|
RU2503585C1 |
| AIRCRAFT BANK ANGLE BANK ANGULAR SPEED LIMITING AUTOMATIC CONTROL SYSTEM | 2010 |
|
RU2430858C1 |
| AUTOMATIC CONTROL SYSTEM OF BANK ANGLE WITH STATIC AUTOPILOT AND WITH LIMITATION OF ANGULAR SPEED OF AIRCRAFT BANK | 2018 |
|
RU2695474C1 |
| AUTOMATIC CONTROL OF BANK ANGLE AND LIMITATION OF BANK ANGULAR SPEED OF AIRCRAFT | 2018 |
|
RU2701628C2 |
| AIRCRAFT PITCH ANGLE BANK ANGULAR SPEED LIMITING AUTOMATIC CONTROL SYSTEM | 2010 |
|
RU2434785C1 |
| AIRCRAFT PITCH ANGLE AND LIMITING PARAMETERS AUTOMATIC CONTROL SYSTEM | 2014 |
|
RU2560958C1 |
| AUTOMATIC CONTROL SYSTEM OF PITCH ANGLE AND LIMITATION OF ANGLE OF ATTACK OF AIRCRAFT | 2018 |
|
RU2686378C1 |
| SYSTEM OF AUTOMATED MODAL CONTROL IN AIRCRAFT LONGITUDINAL AXIS | 2015 |
|
RU2644842C2 |
| SEMIAUTOMATIC SYSTEM FOR PREVENTION OF AIRCRAFT PITCH ANGLE DRIFT BEYOND OPERATING RANGE | 2011 |
|
RU2490168C1 |
| NOISE-PROOF SYSTEM FOR AUTOMATIC CONTROL OF AIRCRAFT BANK ANGLE | 2020 |
|
RU2737872C1 |
