FIELD: aviation.
SUBSTANCE: group of inventions relates to an aircraft control method in response to a yaw movement, a control system for stabilizing an aircraft in response to a yaw movement, to an aircraft comprising such a system. In order to control aircraft, yaw movement is detected, balancing process is initiated, which includes increase of thrust in one or more engines on first side of aircraft and reduction of thrust in one or more engines on aircraft second side, maintaining the thrust difference when the yaw movement is eliminated, repeating the balancing process when it is not excluded. Control system comprises one or more processors and one or more memory devices storing commands for execution of the method.
EFFECT: providing correction of yaw movement without increasing aircraft resistance.
16 cl, 7 dwg
Title | Year | Author | Number |
---|---|---|---|
HYBRID AIRCRAFT | 1996 |
|
RU2160689C2 |
MECHANICALLY DISTRIBUTED POWER PLANT AND METHOD OF AIRCRAFT OPERATION CONTROL | 2019 |
|
RU2743903C2 |
AIRCRAFT AND METHOD OF ITS OPERATION | 2000 |
|
RU2250181C2 |
COAXIAL ROTOR YAW CONTROL | 2014 |
|
RU2684338C2 |
MULTI-COPTER WITH AIR SCREWS OF VARIOUS PURPOSE | 2016 |
|
RU2718460C1 |
METHOD OF WATERCRAFT CONTROL AND WATERCRAFT | 2018 |
|
RU2744812C1 |
AIRCRAFT RESCUE SYSTEM | 2022 |
|
RU2781471C1 |
AIRCRAFT ELECTRONIC CONTROL COMPONENT FOR AIRCRAFT CONTROL UNIT, AIRCRAFT CONTROL UNIT AND AIRCRAFT WITH SAID CONTROL DEVICE | 2010 |
|
RU2537364C2 |
METHOD AND SYSTEM TO CONTROL AIR-CUSHION SHIP | 2009 |
|
RU2399527C1 |
SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL | 2018 |
|
RU2711760C2 |
Authors
Dates
2019-05-21—Published
2017-06-08—Filed