FIELD: data processing.
SUBSTANCE: group of inventions relates to a method and a device for generating control signals for steering drives of an unmanned aerial vehicle. To generate control signals, current control signals are received by course, pitch and roll, aircraft flight speed is measured, kinematic distribution of control signals for steering drives is performed, and rated values of limitation of control signals are set in certain manner. Device comprises three inputs of control signals of flight speed sensor, kinematic distribution unit, setter of nominal values of limitation of control signals, three signal limiters, setpoint of current values of limitation of control signals, connected in certain manner.
EFFECT: higher accuracy of control and expansion of functional capabilities.
2 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
BOARD DIGITAL-ANALOGUE ADAPTIVE SYSTEM OF AIRCRAFT CONTROL | 2009 |
|
RU2391694C1 |
FLYING VEHICLE CONTROL SYSTEM | 2003 |
|
RU2234725C1 |
CONTROL SYSTEM OF PILOTLESS FLIGHT VEHICLE | 2002 |
|
RU2212702C1 |
METHOD FOR FORMING LATERAL-DIRECTIONAL SIGNALS OF NON-STATIONARY UNMANNED AERIAL VEHICLE WITH ADAPTIVE-FUNCTIONAL CORRECTION AND A DEVICE FOR ITS IMPLEMENTATION | 2016 |
|
RU2631736C1 |
DEVICE FOR SHAPING CONTROL SIGNALS FOR FLYING VEHICLE CONTROL SYSTEMS | 2003 |
|
RU2238582C1 |
AIRCRAFT ADAPTIVE COORDINATED CONTROLLER | 2014 |
|
RU2554515C1 |
AIRCRAFT DUAL CHANNEL COORDINATED CONTROLLER | 2013 |
|
RU2532720C1 |
SIMULATOR COMPLEX FOR CHECKING CONTROL SYSTEM OF UNMANNED AIRCRAFT | 2010 |
|
RU2432592C1 |
SYSTEM FOR PREDICTING UNMANNED AIRCRAFT FULL-SCALE TEST RESULTS | 2000 |
|
RU2160927C1 |
SYSTEM FOR CONTROLLING ANGULAR MOTION OF PILOT -FREE AIRCRAFT | 2003 |
|
RU2234117C1 |
Authors
Dates
2019-10-15—Published
2018-11-28—Filed