FIELD: aviation.
SUBSTANCE: group of inventions relates to a method and system for remote control of a two-fin manned aerial vehicle (AV). In order to control the AV in the course channel, pedals, a remote control system (RCS), two steering actuators, two fins with rudders located thereon, two mechanical runs for deflecting the rudders, wherein in order to compensate for the consequences caused by elastic deformations of the fin structures, the coefficient of signal transmission from the outputs of the RCS to the inputs into the steering actuators is changed accordingly. The RCS comprises an air signal system, a pedal movement sensor, a roll control knob movement sensor, sensors of the angle of attack, the angular roll speed, the angular yaw speed, the sliding angle, and the lateral overload, a computing apparatus, left and right steering actuators, mechanical runs for moving the control bodies of the AV in the course channel, left and right rudders, a correction unit, connected in a certain way.
EFFECT: controllability of the manned AV in the course channel is increased over the entire range of permissible ram air values.
3 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
COURSE CHANNEL AIRCRAFT CONTROL SYSTEM | 2021 |
|
RU2768310C1 |
MANNED AIRCRAFT CONTROL SYSTEM WITH ADAPTIVE CROSS LINK | 2019 |
|
RU2736400C1 |
ADAPTIVE SYSTEM FOR CONTROLLING A MANNED AERIAL VEHICLE IN THE ROLL CHANNEL | 2020 |
|
RU2753776C1 |
REMOTE CONTROL SYSTEM OF AIRCRAFT IN LATERAL-DIRECTIONAL MODE | 2017 |
|
RU2671063C1 |
AIRCRAFT LONGITUDINAL CONTROL SYSTEM | 2021 |
|
RU2769452C1 |
AIRCRAFT CONTROL METHOD AND COMPLEX SYSTEM METHOD IS BUILT AROUND | 2006 |
|
RU2327602C1 |
METHOD OF CONTROL OF AIRCRAFT | 2003 |
|
RU2235042C1 |
LIGHT MULTI-MISSION AIRCRAFT | 2003 |
|
RU2235044C1 |
LIMITER OF MANEUVERABLE AIRCRAFT LIMIT MODES OF FLIGHT | 2019 |
|
RU2711040C1 |
METHOD FOR FORMING FAULT-TOLERANT INTEGRATED CONTROL SYSTEM (ICS) AND FAULT-TOLERANT ICS | 2016 |
|
RU2629454C2 |
Authors
Dates
2022-02-03—Published
2020-12-30—Filed