FIELD: physics, control.
SUBSTANCE: invention is related to the field of instrument making and may find application in board systems of automatic control of aircrafts with realisation of coordinated turn modes. In order to achieve this result, control device comprises detector of heeling angle, detector of heeling angular speed, course angle detector, detector of angular speed by course, detector of dynamic head, the first and second summing amplifiers, setter of control signal by course, the first and second subtraction units, inverting amplifier, functional nonlinear element with controlled limitation and nonlinear element with limitation.
EFFECT: expansion of functional resources and high dynamic accuracy of control.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT ADAPTIVE COORDINATED CONTROLLER | 2014 |
|
RU2554515C1 |
| ADAPTIVE DEVICE OF AIRCRAFT COORDINATED CONTROL | 2008 |
|
RU2367992C1 |
| AIRCRAFT DUAL CHANNEL COORDINATED CONTROLLER | 2013 |
|
RU2532720C1 |
| METHOD FOR FORMING LATERAL-DIRECTIONAL SIGNALS OF NON-STATIONARY UNMANNED AERIAL VEHICLE WITH ADAPTIVE-FUNCTIONAL CORRECTION AND A DEVICE FOR ITS IMPLEMENTATION | 2016 |
|
RU2631736C1 |
| METHOD OF GENERATING SIGNAL FOR AIRCRAFT LATERAL GUIDANCE AND DEVICE FOR IMPLEMENTING METHOD | 2007 |
|
RU2339990C1 |
| CONTROL DEVICE FOR SYSTEM OF COORDINATED CONTROL OF FLIGHT VEHICLE | 2003 |
|
RU2237269C1 |
| DEVICE FOR COORDINATED REGULATION OF ANGULAR LATERAL MOVEMENT OF FLYING VEHICLE | 1990 |
|
RU2047888C1 |
| DEVICE FOR COORDINATED CONTROLLING ANGULAR LATERAL MOTION OF AIRCRAFT | 0 |
|
SU1751716A1 |
| DEVICE FOR SHAPING CONTROL SIGNALS FOR FLYING VEHICLE CONTROL SYSTEMS | 2003 |
|
RU2238582C1 |
| BOARD DIGITAL-ANALOGUE ADAPTIVE SYSTEM OF AIRCRAFT CONTROL | 2009 |
|
RU2391694C1 |
