EP2215891A1 - Verfahren zur steuerung eines servosystems - Google Patents

Verfahren zur steuerung eines servosystems

Info

Publication number
EP2215891A1
EP2215891A1 EP08804944A EP08804944A EP2215891A1 EP 2215891 A1 EP2215891 A1 EP 2215891A1 EP 08804944 A EP08804944 A EP 08804944A EP 08804944 A EP08804944 A EP 08804944A EP 2215891 A1 EP2215891 A1 EP 2215891A1
Authority
EP
European Patent Office
Prior art keywords
measurement
offset
control
cycle
measurements
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP08804944A
Other languages
English (en)
French (fr)
Inventor
Sylvain Come
Thierry Ginestet
David Chaillou
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thales SA
Original Assignee
Thales SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Thales SA filed Critical Thales SA
Publication of EP2215891A1 publication Critical patent/EP2215891A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B45/00Circuit arrangements for operating light-emitting diodes [LED]
    • H05B45/10Controlling the intensity of the light
    • H05B45/12Controlling the intensity of the light using optical feedback

Definitions

  • a control device comprises a control chain comprising a sensor measuring a characteristic variable of the system evolving according to a setpoint and a comparator measuring a difference between the setpoint and the value of the variable.
  • the sensor is still called servo sensor.
  • the system is controlled by the difference measured by the comparator.
  • the accuracy of the system response to a setpoint change is generally good. Indeed, the servocontrol tends to cancel the difference between the setpoint and the value of the characteristic variable of the system followed by the servo sensor.
  • the servo chain may experience an offset, hereinafter referred to as "offset", tending to define a non-zero error even if the response of the system is perfectly adapted to the setpoint.
  • the offset can be due to the precision of the components of the servo chain.
  • the offset can change over time as a function of parameters different from the set point influencing the response of the system, parameters such as, for example, the evolution of the ambient temperature or the wear of the components of the servocontrol chain.
  • the invention can be implemented in a backlight control of liquid crystal screens used on aircraft dashboards where it is necessary that the pilot of the aircraft can see these screens regardless of the light ambient of the cockpit.
  • the predominant offset for this backlight application is generated by the ambient lighting of the cockpit, especially when the sun illuminates the liquid crystal screen. A sufficient fraction of ambient illumination is then measured by the internal illumination sensor and comes bias the measurement of it. This parasitic lighting being added to that generated from the backlighting light source, the accuracy of the luminance seen by the driver is degraded.
  • the invention aims to improve the robustness of the control of a slave system by not seeking to minimize the offset but by measuring it in order to compensate for it.
  • the invention is adapted to a slave system by means of a multilevel control cut in time. Indeed, we will use the different levels of system controls to allow the measurement of the offset.
  • the subject of the invention is a method of controlling a slave system by means of a multilevel control cut in time, the method implementing a device receiving a setpoint and comprising a servo chain in which a sensor measures a characteristic variable of the system evolving according to the setpoint, the measurement of the variable being capable of modifying the control of the system through the servocontrol chain, the method being characterized in that it comprises the following operations : • acquire two measurements by means of the sensor, each during a period, the two periods being dissymmetrical with respect to the cutting of the control,
  • the measured offset can be calculated and subtracted from the measurements acquired by the servo sensor by a system of two equations with two unknowns, the two unknowns being the response of the system and the offset of the measurement chain, the two equations being the measures expressed according to the two unknowns.
  • the two equations are not redundant if the two periods are dissymmetrical with respect to the division of the command and thus allow the resolution of the system of equations.
  • the preponderant offset measured by the servo sensor is caused by a physical phenomenon that is interesting to quantify and its value, usually measured by an ancillary system, is used in the definition of the system instruction.
  • the change in the offset is mainly due to variations in ambient lighting, described above as the physical phenomenon.
  • the invention makes it possible to obtain an illumination measurement that is independent of the ambient luminosity.
  • the offset can also be used to adapt the setpoint 1 1 in place of the use of an adjoining sensor for measuring ambient lighting. This makes it possible to use only one sensor for at a time, to slave the control of illumination to the setpoint, and to measure the ambient illumination to generate the setpoint.
  • the setpoint received by the device may be a function of the measured offset.
  • the measurement of the offset mainly due to ambient lighting, is weighted and then added to the setpoint. For example, the illumination setpoint is increased when the ambient brightness increases.
  • FIG. 1 represents in schematic form a slave system for which the invention can be implemented
  • FIGS. 2a to 2d represent, in chronogram form, a command of a system and several examples of measurements making it possible to determine the offset of the servocontrol chain;
  • FIG. 3 represents an example of measurement made by a device according to the invention and makes it possible to eliminate the effect of the offset
  • FIG. 4 represents an exemplary servocontrol chain embodying the invention.
  • FIG. 1 represents an exemplary device for controlling a system 10 as a function of a setpoint 11.
  • the device comprises control means 12 delivering to the system 10 a command 13 through a servo control algorithm.
  • the device further comprises a servo sensor 14 measuring a variable 15 characteristic of the system 10 and evolving as a function of the control 13 and a comparator 1 6 measuring a difference 17 between the setpoint 1 1 and the value of the variable 15. L deviation 17 forms the input data of the control means 12.
  • a method according to the invention is adapted to a multilevel control cut in time.
  • This control is for example cyclic and within one cycle succeeds an active phase during which the system is controlled at a maximum level and an inactive phase during which the system is controlled to a minimum level, for example zero.
  • This type of control is called pulse width modulation control and is well known in the English literature as "Puise With Modulation”.
  • the timing diagram of FIG. 2a denoted PWM, represents the evolution over time of the control of the system 10.
  • the control 13 evolves in two levels. A first low level carries the mark 20 and a second high level carries the mark 21.
  • the system 10 may include light emitting diodes.
  • the low level 20 corresponds to the extinction of the diodes and the high level 21 corresponds to a full power supply of the light emitting diodes.
  • An operating cycle 22 is defined between two rising edges 23 and 24 forming transitions from level 20 to level 21. According to the invention, the method comprises the following operations:
  • the timing diagram of Figure 2b represents an example of implementation of the two periods.
  • the period of the first measurement 31 extends over the duration of the active phase and the period of the second measurement 32 extends over the duration of the inactive phase.
  • the first measurement 31 is carried out as long as the control 13 is high 21 and the second measurement 32 is performed as long as the control 13 is at the low level 20.
  • the synchronization of the two measurements 31 and 32 on the levels 20 and 21 can be done by the control means 12 which further determine the transitions between the levels 20 and 21.
  • the offset is determined directly by the value measured by the sensor 14 during measurement 32.
  • the determination of the response of the system 10 to the control 13 is made in deducing the offset from the value measured by the sensor 14 during measurement 31.
  • This type of determination is simple to implement. Nevertheless, the duration of the measurements depends on the duty cycle and can make measurements inaccurate when the duty ratio is close to 0% or close to 100%. Indeed, in these two cases, one of the two measurements 31 or 32 is performed for a much shorter duration than the other and the shortest measurement is therefore more imprecise than the other.
  • FIGS. 2c and 2d Two other examples of implementation of a method according to the invention are illustrated by the timing diagrams of FIGS. 2c and 2d and make it possible to improve the accuracy of the determination of the offset and of the response of the system by lengthening the periods of measure beyond a given value.
  • measurement periods span at least half of the cycle.
  • the period of a first measurement 33 extends over a complete cycle and the period of a second measurement 34 extends over a final half-cycle.
  • Measure 33 can be expressed as follows:
  • R system represents the response of the system and offset cy ts representing the offset on a full cycle.
  • Measurement 34 depends on the duty cycle. If this ratio is less than 50%, the measure 33 can be expressed as follows:
  • measure 33 can be expressed as follows:
  • M short R system ⁇ 1/2 R max system + OffSte 1/2 cycle (3)
  • R max system representing the response of the system for a duty cycle of 100%.
  • system R system response can be expressed according to:
  • Offset cycle 2 X Offset 1/2 cycle (7)
  • Offset cycle M long "R system (1 0)
  • the offset thus defined can be used to define the control 11 for example in the case of an implementation of the invention for the backlight of a screen considering that the predominant offset is related to the ambient brightness.
  • Figure 3 shows an orthogonal reference two curves 40 and 41 superimposed.
  • the curve 40 shown in fine lines, expresses the response of the system R system according to the duty cycle noted PWM.
  • the PWM duty cycle changes from 0% to 100%.
  • Curve 40 is a line segment extending from an origin 42 of the marker to a point 43 associating the maximum response of system R max system to a duty cycle of 100%.
  • the curve 41 represents, in the same reference, the difference between the measurement 33, long M, and twice the measurement 34, short M, as a function of the duty cycle PWM in the form of a curve 41 in solid line.
  • the curve 41 is formed of two line segments 44 and 45.
  • the segment 44 extends from the origin 42 of the marker to a point 46 associating half of the maximum system response, Vz R max system, to a cyclical ratio of 50%.
  • the segment 44 is superimposed on the curve 40.
  • the segment 45 extends from the point 46 to a point 47 associating a difference between the measurement 33, M bngue, and twice the measurement 34, M short, zero to one cyclical ratio of 100%.
  • the period of a first measurement 35 extends over an initial half-cycle and a second measurement 36 extends over a final half-cycle.
  • a calculation mode similar to the previous one can be implemented to determine the offset and the response of the system by eliminating the effect of the offset.
  • FIG. 4 represents an example of a servo-control chain adapted to the measurements 33 and 34 of FIG. 2c implementing the invention.
  • An alternative of a method according to the invention consists in carrying out the two measurements during the same cycle.
  • the two measurements can overlap or not. Overlap will intervene compulsorily in combination with the variant described with the help of Figure 2c since the measurement 33 already occupies the entire cycle.
  • the measurement 34 is performed during the second half of the same cycle. Performing both measurements during the same cycle limits the effects of an offset that may change over time.

Landscapes

  • Feedback Control In General (AREA)
  • Liquid Crystal Display Device Control (AREA)
  • Circuit Arrangement For Electric Light Sources In General (AREA)
  • Control Of Indicators Other Than Cathode Ray Tubes (AREA)
  • Control Of Position Or Direction (AREA)
EP08804944A 2007-10-02 2008-10-01 Verfahren zur steuerung eines servosystems Withdrawn EP2215891A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0706900A FR2921733B1 (fr) 2007-10-02 2007-10-02 Procede de commande d'un systeme asservi
PCT/EP2008/063119 WO2009043863A1 (fr) 2007-10-02 2008-10-01 Procede de commande d'un systeme asservi

Publications (1)

Publication Number Publication Date
EP2215891A1 true EP2215891A1 (de) 2010-08-11

Family

ID=39262565

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08804944A Withdrawn EP2215891A1 (de) 2007-10-02 2008-10-01 Verfahren zur steuerung eines servosystems

Country Status (5)

Country Link
US (1) US8258855B2 (de)
EP (1) EP2215891A1 (de)
CN (1) CN101843171B (de)
FR (1) FR2921733B1 (de)
WO (1) WO2009043863A1 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2524233A (en) 2014-03-04 2015-09-23 Nokia Technologies Oy A method, apparatus and/or computer program for controlling light output of a display
CN106292275B (zh) * 2015-05-29 2019-02-26 明纬(广州)电子有限公司 基于开关机纪录的自适性调控方法
JP6799804B2 (ja) * 2015-09-10 2020-12-16 パナソニックIpマネジメント株式会社 照明装置及びそれを備えた照明システム、移動体
DE102018212529A1 (de) * 2018-07-27 2020-01-30 Robert Bosch Gmbh Verfahren und Steuergerät zum Regeln einer emittierten Lichtleistung einer Lichtquelle eines optischen Sensorsystems

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6441558B1 (en) * 2000-12-07 2002-08-27 Koninklijke Philips Electronics N.V. White LED luminary light control system
DE10227487B4 (de) * 2002-06-19 2013-11-21 Wilo Se Beleuchtungsvorrichtung
US7656100B2 (en) * 2004-07-23 2010-02-02 Koninklijke Philips Electronics, N.V. System for temperature prioritised colour controlling of a solid-state lighting unit
WO2006111689A1 (en) * 2005-04-21 2006-10-26 Radiant Research Limited Illumination control system for light emitters
EP1891837A2 (de) * 2005-05-27 2008-02-27 Koninklijke Philips Electronics N.V. Steuerung einer anordnung von halbleitern, die licht verschiedener farbe emittieren
US7755349B2 (en) * 2008-03-03 2010-07-13 Memsic, Inc. Correcting offset in magneto-resistive devices

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2009043863A1 *

Also Published As

Publication number Publication date
CN101843171B (zh) 2012-12-26
US8258855B2 (en) 2012-09-04
US20110050147A1 (en) 2011-03-03
FR2921733A1 (fr) 2009-04-03
WO2009043863A1 (fr) 2009-04-09
CN101843171A (zh) 2010-09-22
FR2921733B1 (fr) 2010-02-26

Similar Documents

Publication Publication Date Title
EP0406116B1 (de) Verfahren und Vorrichtung zum Dimmen einer Leuchtstofflampe in einer LCD-Anzeigen-Rückbeleuchtung
EP0041882B1 (de) Einrichtung zum Voreinstellen der Frequenz einer indirekten Frequenzsyntheseschaltung und eine solche Einrichtung enthaltende Frequenzsyntheseschaltung
EP2215891A1 (de) Verfahren zur steuerung eines servosystems
EP2959300B1 (de) Sensor mit einem elektrostatischen pendelartigen beschleunigungsmesser und verfahren zur steuerung solch eines sensors
CA2910558C (fr) Procede et dispositif de generation d'une commande de debit de carburant destine a etre injecte dans une chambre de combustion d'une turbomachine
FR2509548A1 (fr) Generateur de signaux triangulaires comportant un circuit de compensation du retard de la boucle
CA2877210A1 (fr) Procede et dispositif d'ajustement d'une valeur seuil de debit carburant
WO2021023576A1 (fr) Procédé d'analyse d'un gaz par un capteur optique
EP2416625B1 (de) Verfahren zur Steuerung von Leuchtdioden
JP2009212422A (ja) 半導体発光素子の制御
FR2994606A1 (fr) Procede et dispositif de commande de puissance ou de tension d'un consommateur electrique
CH698856B1 (fr) Système de régulation d'un portique à double moyen d'entraînement.
FR2488696A1 (fr) Procede et dispositif de detection du decollement tournant apparaissant dans une turbomachine a deux corps tournants
EP4154047A1 (de) Abgetastetes lichtbündelvideoprojektionssystem und verfahren, head-up-anzeige in einem kraftfahrzeug und adaptive beleuchtungsvorrichtung mit solch einem system
EP1406141B1 (de) Verfahren und Einrichtung zur automatischen Steuerung des Schubes eines Flugzeugantriebes
FR2862714A1 (fr) Procede et dispositifs de surveillance d'un systeme d'injection d'un moteur a combustion interne
FR2976150A1 (fr) Dispositif de commande de diodes electroluminescentes a tres grande dynamique de luminance pour ecran de visualisation
EP2862036B1 (de) Vorrichtung zur versorgung eines elektronischen stromkreises
WO2019207244A1 (fr) Procédé et système de traitement d'un signal de mesure d'une température délivré par un capteur
FR3090257A1 (fr) Procédé de capture d’images adapté aux sources lumineuses scintillantes et capteur d’images
US20240319348A1 (en) Time-of-flight camera system
WO2014087103A1 (fr) Procédé et dispositif embarque d'analyse de fluide dans un moteur thermique
FR3143818A1 (fr) Procédé de détermination d'un état d'un écran
EP3357753B1 (de) Fahrerassistenzverfahren und -system
EP2469988B1 (de) Helligkeitsmaß an der Decke

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20100423

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

DAX Request for extension of the european patent (deleted)
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20150501