FIELD: automatic systems.
SUBSTANCE: invention relates to systems and methods for automatic system control. A method for automatically adjusting includes measuring of plurality of characteristic parameters of the system, in which one of the parameters (u) is used as a control function of the measured values (y). Next, choose a nominal operating point of the system, determine the nominal model (Mn), describing the system in the nominal operating point, and the calculated output parameters characteristic (yr) corresponding to a measurable characteristic parameter (y) are determined from said nominal model, determine the error between a measured characteristic output parameter (y) and one of the estimated output characteristic parameters. One of the control parameters of the system are used as the error function defined to reduce the error between a calculated output characteristic parameters (yr) and the corresponding one measured characteristic value of the measured output parameter (y).
EFFECT: achieved by the possibility of reducing the state system disturbances.
14 cl, 7 dwg
Title | Year | Author | Number |
---|---|---|---|
CONTROL METHOD | 2012 |
|
RU2552891C1 |
METHOD AND DEVICE FOR CONTROLLING A GUIDED MISSILE BY MEANS OF A DRIVE WHICH TRACKS ORIENTATION OF TRAJECTORY | 2003 |
|
RU2323464C2 |
METHOD FOR CONTROL OF NUCLEAR REACTOR OPERATING PARAMETERS AND CORRESPONDING NUCLEAR REACTOR | 2019 |
|
RU2794140C2 |
METHOD AND DEVICE FOR THE ROCKET ENGINE PARAMETER MONITORING | 2015 |
|
RU2654310C2 |
METHOD AND DEVICE FOR CALCULATION OF INSTANTANEOUS ROTARY SPEED OF BOTTOMHOLE ASSEMBLY | 2012 |
|
RU2518699C1 |
METHOD AND APPARATUS FOR SUPPRESSING NARROW-BAND NOISE IN PASSENGER CABIN OF VEHICLE | 2009 |
|
RU2504025C2 |
METHOD AND DEVICE TO CALCULATE INSTANTANEOUS SPEED OF DRILLING STRING ASSEMBLY BOTTOM ROTATION | 2009 |
|
RU2478782C2 |
METHOD OF COMPLEX RECTIFICATION COLUMN OIL PRIMARY PROCESS CONTROL | 1990 |
|
RU2040294C1 |
METHOD OF CONTROLLING TOWING SYSTEM (TOW AIRCRAFT -TOWING CABLE - TOWED AIRCRAFT) | 2007 |
|
RU2347719C1 |
METHOD OF RECONSTRUCTING LOADS CAUSED BY GUST AND/OR LOADS ON AIRCRAFT AIRFRAME, IN PARTICULAR, THAT OF PASSANGER AIRLINER | 2006 |
|
RU2413658C2 |
Authors
Dates
2016-05-27—Published
2012-07-20—Filed