FIELD: physics; aviation.
SUBSTANCE: group of inventions relates to a method and device for generating a steering signal control signal of an unmanned aerial vehicle (UAV). To generate a control signal, they set a control signal, amplify it and limit it, filter the subtraction signal, amplify the filtered signal, form the current speed signal deflection steering and scale it, work out the current signal deflection steering actuator, while additionally measure the velocity head, angle of attack, coefficient of efficiency of the hinge moment from the angle of attack and from the rudder deviation, form the current speed signal taking into account its insensitivity in the zone of the current value of the hinge moment in a certain way. Device contains a control signal adjuster, two signal amplifiers, a signal limiter, two subtraction elements, an inertial filter, an actuator and an actuator, a deflection angle signal sensor, a deflection speed signal sensor, an inertial amplifier, sensors of velocity head and angle of attack, sets of efficiency factor for articulated torque from steering deflection and angle of attack, two multipliers, summing amplifier, amplifier with non-sensibility zone, connected in a certain way.
EFFECT: provides enhanced functionality and improved control accuracy of the UAV.
2 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR CONTROLLING FRICTION ELECTRIC DRIVE OF AIRCRAFT | 2004 |
|
RU2263338C1 |
METHOD OF GENERATING INTEGRAL ADAPTIVE SIGNAL FOR STABILISING GLIDING MOTION OF UNMANNED AIRCRAFT AND APPARATUS FOR REALISING SAID METHOD | 2011 |
|
RU2460113C1 |
METHOD OF FORMATION OF ADAPTIVE SIGNAL OF CONTROL AND STABILISATION OF ANGULAR MOVEMENT OF AIRCRAFT, AND DEVICE FOR ITS IMPLEMENTATION | 2013 |
|
RU2569580C2 |
DEVICE FOR COORDINATED REGULATION OF ANGULAR LATERAL MOVEMENT OF FLYING VEHICLE | 1990 |
|
RU2047888C1 |
METHOD FOR FORMING LATERAL-DIRECTIONAL SIGNALS OF NON-STATIONARY UNMANNED AERIAL VEHICLE WITH ADAPTIVE-FUNCTIONAL CORRECTION AND A DEVICE FOR ITS IMPLEMENTATION | 2016 |
|
RU2631736C1 |
MODELING COMPLEX FOR DEBUGGING CONTROL SYSTEM OF AUTONOMOUS MOBILE UNIT | 2017 |
|
RU2662331C1 |
BOARD DIGITAL-ANALOGUE ADAPTIVE SYSTEM OF AIRCRAFT CONTROL | 2009 |
|
RU2391694C1 |
AIRCRAFT ADAPTIVE COORDINATED CONTROLLER | 2014 |
|
RU2554515C1 |
ONBOARD ANGULAR STABILISATION SYSTEM FOR CONTROLLING FLYING AIRCRAFT | 2007 |
|
RU2338236C1 |
ADAPTIVE DEVICE TO GENERATE SIGNAL CONTROLLING AIRCRAFT LENGTHWISE-EQUALISING MOTION | 2009 |
|
RU2394263C1 |
Authors
Dates
2019-03-12—Published
2018-06-26—Filed