FIELD: instrument making.
SUBSTANCE: control system comprises setters of pitch, course and list angles, the first, second and third comparison units, unit of free gyroscopes, unit of damping gyroscopes, speed and flight altitude sensors, sensor of current mass value, setter of reference signals, the first and second multiplication units, the first and second units of division, summator, unit of generation of reverse signal value, scaling unit, digital multiplication unit, digital-analogue converter, digital-analogue multiplication unit, the first, second and third summing amplifiers and executive device.
EFFECT: expansion of functional capabilities.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
ONBOARD DIGITAL-ANALOG ADAPTIVE SYSTEM FOR CONTROLLING BANKING MOVEMENT OF AIRCRAFT | 2005 |
|
RU2305308C1 |
METHOD OF GENERATING DIGITAL/ANALOGUE ADAPTIVE SIGNAL FOR STABILISING ANGULAR POSITION OF AIRCRAFT ON HEADING AND APPARATUS FOR REALISING SAID METHOD | 2012 |
|
RU2491600C1 |
MULTIMODE D/A DRONE ANGULAR PITCH CONTROL DEVICE | 2014 |
|
RU2541903C1 |
ONBOARD ANGULAR STABILISATION SYSTEM FOR CONTROLLING FLYING AIRCRAFT | 2007 |
|
RU2338236C1 |
METHOD OF GENERATING DIGITAL-ANALOG ADAPTIVE CONTROL SIGNAL FOR DRONE ANGULAR MOTION ONBOARD CONTROL SYSTEMS AND DEVICE TO THIS END | 2012 |
|
RU2469373C1 |
METHOD OF FORMATION OF ADAPTIVE SIGNAL OF CONTROL AND STABILISATION OF ANGULAR MOVEMENT OF AIRCRAFT, AND DEVICE FOR ITS IMPLEMENTATION | 2013 |
|
RU2569580C2 |
ADAPTIVE SYSTEM FOR CONTROLLING FLIGHT HEIGHT OF AN AIRCRAFT | 2005 |
|
RU2279119C1 |
SYSTEM FOR INCREASING SMALL AIRCRAFT FLIGHT SAFETY | 2009 |
|
RU2413274C1 |
METHOD OF FORMING A CONTROL SIGNAL OF A STEERING DRIVE OF AN UNCLEANED AIRCRAFT AND A DEVICE FOR ITS IMPLEMENTATION | 2018 |
|
RU2681823C1 |
ADAPTIVE SYSTEM WITH REFERENCE MODEL FOR CONTROL OF AIRCRAFT | 2016 |
|
RU2647405C1 |
Authors
Dates
2010-06-10—Published
2009-04-15—Filed