FIELD: aviation; control systems.
SUBSTANCE: group of inventions relates to a method and a system for controlling the trajectory long run on a flight strip and a climbing of the unmanned aerial vehicle (UAV) with the front and rear wings articulated on the keel. To implement the method, based on the results of preliminary simulation of UAV longitudinal movement in the calculation unit, analytical dependencies and values of all parameters required during model testing are generated, required parameters are measured and selected to smooth rudder oscillations and avoiding short-term detachments from the flight strip, which ensures fast climb when sufficient lifting force is achieved. Control system comprises in-series correcting links of steering contours wheels of front and rear wings. Contour of rear wing rudders control comprises measurement unit, oscillating link, nonlinear link with linearity zone and angular speed limitation, differentiating link, adder, aperiodic link, nonlinear link with linear zone and rudder height limitation. Contour of rudders control of front fenders includes unit of calculations, contour compares link by angle of attack, amplifier by angle of attack, adder, aperiodic link, nonlinear link with linear zone and rudder limitation height, connected in certain manner.
EFFECT: higher AC stability at flight strip run area and climbing.
2 cl, 7 dwg
Title | Year | Author | Number |
---|---|---|---|
SMART CREW SUPPORT SYSTEM | 2015 |
|
RU2598130C1 |
INTELLIGENT SYSTEM OF CREW SUPPORT | 2013 |
|
RU2541902C2 |
UNMANNED FLYING VEHICLE | 2005 |
|
RU2288140C1 |
ON-BOARD INTEGRATED CREW SUPPORT INFORMATION SYSTEM AND COGNITIVE FORMAT OF PRESENTING FLIGHT INFORMATION AT TAKE-OFF PHASE OF MULTI-ENGINE AIRCRAFT | 2013 |
|
RU2550887C2 |
MULTI-PURPOSE TWIN-ENGINED SEA-BASED AND LAND- BASED AIRCRAFT OF SHORT TAKEOFF AND LANDING | 2001 |
|
RU2196707C2 |
AMPHIBIAN AIRCRAFT PITCH ANGLE CONTROL SYSTEM DURING MOTION IN WATER IN HYDROPLANING MODE | 2004 |
|
RU2268157C1 |
METHOD OF DISTRIBUTION-FREE IDENTIFICATION OF NONLINEAR AERODYNAMIC CHARACTERISTICS OF AIRCRAFT BY FLIGHT TEST RESULTS | 2014 |
|
RU2560244C1 |
FLIGHT VEHICLE (VERSIONS), FLIGHT VEHICLES PARTS, METHOD OF EXPLOITING FLIGHT VEHICLE AND ITS PARTS | 2010 |
|
RU2466061C2 |
AIRCRAFT AERODYNAMIC CONFIGURATION | 1994 |
|
RU2090445C1 |
SYSTEM OF AUTOMATED MODAL CONTROL IN AIRCRAFT LONGITUDINAL AXIS | 2015 |
|
RU2644842C2 |
Authors
Dates
2019-07-29—Published
2018-10-26—Filed