FIELD: control systems; coding.
SUBSTANCE: group of inventions relates to a method and apparatus for generating a digital-analog signal of angular stabilization of a non-stationary control object. To generate an angular stabilization signal, a digital signal of angular position is set, measure the digital signal of the angular position, form its lag, an analog signal of the angular velocity is measured, a digital error signal is generated and converted into an analog signal, the output of the angular velocity is formed, the velocity head signal is measured, the delay signal is delimited in a certain manner, the minimum velocity head signal is set, set the minimum level of the signal for limiting the total signal at values of the velocity head equal to or less than the minimum. Device contains a digital angle sensor, an angular velocity sensor, a digital angle adjuster, a digital comparator, a digital-to-analog converter, summing amplifier, actuator, delay element, high-speed head sensor, three adaptive signal limiters, a unipolar relay element, a controllable switch, a minimum speed head signal selector connected in a certain way.
EFFECT: improved accuracy and quality of management of the non-stationary control object.
2 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR FORMING MULTIFUNCTIONAL SIGNAL OF AIRCRAFT ANGULAR POSITION STABILISATION AND DEVICE FOR ITS IMPLEMENTATION | 2016 |
|
RU2631718C1 |
MULTIMODE D/A DRONE ANGULAR PITCH CONTROL DEVICE | 2014 |
|
RU2541903C1 |
METHOD OF DRONE ANGULAR POSITION STABILIZING NON-LINEAR ADAPTIVE DIGITAL/ANALOGUE SIGNAL GENERATION AND STABILIZATION SYSTEM FOR ITS IMPLEMENTATION | 2015 |
|
RU2601089C1 |
METHOD OF GENERATING DIGITAL/ANALOGUE ADAPTIVE SIGNAL FOR STABILISING ANGULAR POSITION OF AIRCRAFT ON HEADING AND APPARATUS FOR REALISING SAID METHOD | 2012 |
|
RU2491600C1 |
METHOD OF GENERATING DIGITAL-ANALOG ADAPTIVE CONTROL SIGNAL FOR DRONE ANGULAR MOTION ONBOARD CONTROL SYSTEMS AND DEVICE TO THIS END | 2012 |
|
RU2469373C1 |
METHOD OF GENERATING DIGITAL/ANALOGUE ADAPTIVE AIRCRAFT CONTROL SIGNAL WITH VARIABLE STRUCTURE AND APPARATUS FOR REALISING SAID METHOD | 2012 |
|
RU2491601C1 |
METHOD FOR FORMING LATERAL-DIRECTIONAL SIGNALS OF NON-STATIONARY UNMANNED AERIAL VEHICLE WITH ADAPTIVE-FUNCTIONAL CORRECTION AND A DEVICE FOR ITS IMPLEMENTATION | 2016 |
|
RU2631736C1 |
METHOD OF GENERATING INTEGRAL ADAPTIVE SIGNAL FOR STABILISING GLIDING MOTION OF UNMANNED AIRCRAFT AND APPARATUS FOR REALISING SAID METHOD | 2011 |
|
RU2460113C1 |
ADAPTIVE SYSTEM FOR CONTROLLING FLIGHT HEIGHT OF AN AIRCRAFT | 2005 |
|
RU2279119C1 |
BOARD DIGITAL-ANALOGUE ADAPTIVE SYSTEM OF AIRCRAFT CONTROL | 2009 |
|
RU2391694C1 |
Authors
Dates
2018-05-08—Published
2017-07-10—Filed