Abstract:
A method of adaptively controlling the time of rendering the individual controlled devices of a controllable power conversion bridge includes the sensing of the instant in time at which the current from the bridge to a load becomes discontinuous. From the time of this sensing, the time period to a predetermined time such as a normally calculated time of rendering the controlled devices conductive is derived. This time period is then multiplied by a multiplier and the resultant product is combined with the predetermined time to provide an actual time of rendering the controlled devices conductive.

Description:
BACKGROUND OF THE INVENTION 
     The present invention relates generally to power conversion apparatus and more particularly to a method of developing a linear relationship between the load voltage of a controlled converter bridge and a command which determines that load voltage. 
     It is common practice in the discipline of power conversion to use a bridge arrangement of controllable devices, such as thyristors or transistors, to provide an output voltage of controllable magnitude and/or frequency. Such bridge arrangements are most commonly used to convert alternating current (AC) electrical power to direct current (DC) electrical power or DC power to AC power, although similar arrangements for AC to AC and DC to DC are also known. In these converters, the several controllable elements are sequentially rendered conductive in some predetermined order to effect the desired output of the converter. 
     Perhaps the most common form of converter in use today, at least in the higher power fields, is the thyristor bridge converter. Employing well known phase control techniques, thyristor converters are able to provide electrical power outputs of controllable magnitude and/or frequency. An ideal control for such a converter would be one which causes the load voltage to be linearly proportional to a command voltage. One problem associated with these bridge converters, as well as some other types, is that they tend to exhibit a non-linear relationship between their load voltage and the command (a command voltage or reference). 
     The most common technique in use today for adjusting for this non-linearity is through the use of &#34;biased cosine&#34; firing logic, an example for which is described in Chapter 10 of Thyristor Phase-Controlled Converters and Cycloconverters by Brian R. Pelly - Wiley Interscience, Copyright 1971, Library of Congress Catalog Card Number 70-125276 which publication is specifically incorporated hereinto by reference. This biased cosine firing technique, although not one hundred percent effective performs adequately for most purposes so long as the converter output current remains continuous. It has been found, however, that when the current becomes discontinuous, the non-linearity between the load voltage and the command voltage or reference substantially increases. 
     SUMMARY OF THE INVENTION 
     It is, therefore, an object of the present invention to provide an improved method for enhancing the linear relationship between the load voltage of a controlled converter bridge and the applied command by adjusting the time of rendering the controlled elements of the bridge conductive. 
     It is a further object to provide a method for correcting for differences in the conduction angle of the controlled elements of a control rectifier bridge which method is suitable for a computer type application. 
     It is another object to provide an improved method for enhancing the linear relationship between the load voltage of a controlled converter bridge and the command voltage or reference when said bridge converter is operating in the discontinuous current mode. 
     The foregoing and other objects are achieved, in accordance with the present invention, by the method of first sensing the time at which the load current becomes discontinuous and, in response to that sensing of time, determining the time period between that time and a predetermined time (e.g., a normally calculated time for rendering of the next said controlled device conductive based upon a presumption of continuous current from the converter) which is not later than the time of rendering the next controlled device conductive. This time period is multiplied by a predetermined multiplier determined by parameters of the converter bridge and the load to give a time interval which is utilized to develop a time for the actual firing of the controlled devices within the bridge. 
    
    
     BRIEF DESCRIPTION OF THE DRAWING 
     While the present invention is described in particularity in the claims annexed to and forming a part of this specification, a better understanding of the invention can be had by reference to the following description taken in conjunction with the accompanying drawing in which: 
     FIG. 1 is a schematic block diagram illustrating a typical environment for application of the method of the present invention; 
     FIG. 2 shows a voltage wave shape helpful in understanding the present invention; and, 
     FIG. 3 is a flow diagram describing the method of the present invention. 
    
    
     DETAILED DESCRIPTION 
     Referring now to FIG. 1, there is shown in schematic form a suitable environment for employing the present invention. As illustrated, a six-pulse AC to DC converter 10, including six thyristors 1 through 6, receives three phase AC power from a source illustrated by the three lines L 1 , L 2  and L 3 . The order of firing or rendering conductive of the several thyristors in the bridge is in the sequence of their numbering as shown. A DC output is provided by the bridge on conductors 12 and 14 to a suitable load 16, for example, a DC motor. The actual firing or rendering conductive of the several thyristors of the bridge 10 is from firing circuits 18 by way of suitable conductors to the gate electrodes of the thyristors 1 through 6 as illustrated by lines 23. In FIG. 1, only two such lines to the gating electrodes have been shown for sake of simplicity, it being expressly understood each of the gate electrodes would be similarly connected. 
     As illustrated, the actual output of the firing circuits 18 is under the control of a suitable computer 20 which may be, for example, an Intel 8085 which includes, for purposes to be discussed later, a counter 22. Computer 20, responds to an input command signal on line 21 in accordance with a pre-established program; e.g., the biased cosine method as described in the forementioned publication by Pelly, and serves to compute the appropriate firing angles for the thyristors of the bridge 10 as modified in accordance with the present invention. A typical computer controlled implementation is described in U.S. Pat. No. 4,090,116, &#34;Closed Loop Digital Control System and Method for Motor Control&#34;, by D. L. Lippitt issued May 16, 1978, which patent is specifically incorporated hereinto by reference. The signal path from the computer 20 to firing circuits 18 is illustrated by lines 24. 
     In order to implement the adaptive control of the subject invention, there is provided some means to determine when the current from the bridge 10 to the load 16 (the load current) becomes discontinuous. In this regard there is shown, in full line form, a detector 26 which is connected across the conductors 12 and 14 by way of lines 25. Detector 26 will provide an output signal by way of line 28 to the computer 20 and more particularly to the counter 22 of that computer in order to initiate a beginning of a count. Preferably, detector 26 is that which is shown and described in co-pending application Ser. No. 458,109, &#34;Commutation Detector Scheme&#34; by William D. Brackman, Jr., (which is assigned to the assignee of the present invention), filed on Jan. 14, 1983. Other forms of detecting discontinuous current, however, may be used. As another example, in FIG. 1 there is shown in phantom form, a current transformer 30 which is connected by way of a line 32 to the detector 26. As a further example of detecting discontinuous current, the voltage across each of the several thyristors 1 through 6 of the bridge 10 could be monitored to determine when each of the voltages is high to thus determine that the bridge is not conducting and hence the current is discontinuous. The primary function to be achieved is to determine a discontinuous current to provide an output signal via line 28 to the counter portion 22 of the computer 20 to initiate a count for reasons which will be explained. 
     With the foregoing in mind, prior to discussing the method of the present invention, it is advisable to reference FIG. 2 which illustrates a typical load voltage wave shape such as might be provided by the converter 10 of FIG. 1 with a firing angle of approximately 100 degrees following the crossings of the phase voltages of the source L 1 , L 2  and L 3  of the zero axis. 
     Three points in time and two time periods are pertinent to this discussion. Time β O  represents the point in time at which the current actually becomes discontinuous (goes to zero) as would be determined by the detector 26 (FIG. 1). β F  represents the actual firing time in accordance with the practice of the present invention. Time β C  represents some predetermined time between β O  and β F  for determining a time interval for the practice of the method of the present invention. In accordance with the specific preferred embodiment, β C  represents that time at which the normal biased cosine type of firing control would calculate as an appropriate time to render the next thyristor conductive based upon an assumption of continuous current. This is in accordance with the aforementioned publication by Pelly. As illustrated, t 1  is the period of time between β O  and β C , while t 2  is the time interval between β C  and β F . Thus, in accordance with the present embodiment as will be discussed in detail with respect to FIG. 3, the β O  time is sensed to initiate operation of counter 22 (FIG. 2) and the time period t 1  is then determined from the count in counter 22 at time β C . Interval t 2  is then calculated using period t 1  and t 2  is then added to time β C  to define the time for the actual firing of the thyristors; i.e., time β F , is determined. 
     Referencing now FIG. 3, in conjunction with the previously discussed FIGS. 1 and 2, it is seen that, in accordance with the method of the present embodiment, at time β O  there is provided an output signal from detector 26 via line 28 such as to start counter 22 of computer 20. At time β C , the count contained in counter 22 is read. Since the adaptive control of the present invention is, like any adaptive control, subject to certain limitations, if the count in the counter is greater than some preset value, that preset value is used. The count thus achieved, representing time period t 1 , is then scaled to properly correspond to the firing delay hardware of the biased cosine computation. This firing delay hardware could include, for example, counter 224 as shown in the aforementioned U.S. Pat. No. 4,090,116. 
     The next step in the present embodiment is to calculate the time interval t 2 . This is done in accordance with the relationship; t 2  =K·t 1 , wherein K is a constant for the given application and related to the load time constant and the configuration of the overall system. In accordance with this preferred embodiment of the present invention, the constant K is defined by the expression: 
     
         K=(1-e.sup.-kNωt.sbsp.M) 
    
     wherein: 
     e=2.71828 
     k=constant, usually less than unity, 
     N=number of active bridge semiconductors (six as shown in FIG. 1) 
     ω=power source frequency in radians 
     t M  =load time constant (e.g., the RL time constant of the load). 
     After t 2  is computed, that time interval is added to the β C  time to generate or develop, within computer 20, the new firing time β F . This β F  time is then set up in the firing delay hardware for firing the thyristors of the bridge 10 to thus provide a new firing time. At time β F  when the next controlled device is fired, the counter is initialized; i.e., is set to zero or whatever preset value is being used in anticipation of the next commutation event. This subroutine will then be repeated for each firing of the several devices of the bridge 10. The actual program for implementing the subroutine as illustrated by FIG. 3 is shown in Appendix A which is attached to and forms a part of this specification. 
     It is also possible that a new value of β F  (i.e., β F  &#39;) may be updated for intermediate values of β C  (β C  &#39;) which are repeatedly updated until the time of β F . This may be done in accordance with the formula in the form of: 
     
         β.sub.F &#39;=(t.sub.1 +(β.sub.C &#39;-β.sub.C))K+β.sub.C &#39;. 
    
     Such an adaptive update in accordance with the above formula for the new calculation β F  &#39; will provide minimum transportation delay and thus maximum response. A less precise updating technique would be to retain the value of t 2  and sum that retained value with the latest β C  value (β C  &#39;) in accordance with the relationship: β F  &#39;=t 2  +β C  &#39;. 
     From the foregoing, it is seen that there has been provided a system which is easily implemented and will greatly enhance linearity between the load voltage of a converter bridge and the command voltage or reference when the current becomes discontinuous for any reason. 
     While there has been shown and described what is at present considered to be the preferred embodiment of the present invention, modifications thereto will readily occur to those skilled in the art. For example, while the specific preferred embodiment utilized the normally calculated firing time to define β C , β C  could be defined by other methods such as a fixed period of time (e.g., 60 electrical degrees) after the firing of the most recently fired controlled device. It is not desired, therefore, that the invention be limited to that specifically shown and described and it is intended to cover in the appended claims all such modifications as fall within the true spirit and scope of the invention. 
     
                                           APPENDIX A__________________________________________________________________________402         ADAPT403404         ADAPT            TO CONDUCTION ANGLE.                           ELSE405 003E 3A 00 00     E      LDA U3CNTO     READ EXTINCTION ANGLE COUNTER406 0041 FE D3   CPI 0D3H407 0043 D2 48 00     C      JNC CNTOK      IF COUNT &lt; D3H, THEN408         ADPTO409 0046 3E D3   MVI A, 0D3H    SUBSTITUTE D3H410         CNTOK               ENDIF411 0048 2F      CMA            CHANGE SIGN412 0049 A7      ANA A          SCALE TO MATCH PLLCMP413 004A 1F      RAR414 004B A7      ANA            MULTIPLY BY GAIN OF 0.75415 004C 1F      RAR416 004D 5F      MOV E,A417 004E A7      ANA A418 004F 1F      RAR419 0050 8B      ADC E420 0051 5F      MOV E,A421 0052 32 00 00     E      STA TMZERO     UPDATE TMZERO TO ACTUAL VALUE422 0055 FE 01   CPI 1423 0057 DA 84 00     C      JC OKFIR       IF TMZERO &lt;1 , GOTO OKFIR424 005A 16 00   MVI D,00H425                             END IF426 005C 2A 0000     E      LHLD TTFIR     ADD TO &#34;TIME TO FIRE&#34;427 005F 19      DAD D428                             IF RESULT &gt; 360 DEG, THEN429 0060 EB      XCHG430 0061 21 80 FE            LXI H,0FE80H   IFE80H = -360 DEG431 0064 19      DAD D432 0065 DA 69 00     C      JC ADPT1433 0068 EB      XCHG           SUBTRACT 360 DEG434         ADPT1               ENDIF435 0069 22 00 00     E      SHLD PLLCMP    SET UP ADJUSTED PLLCMP VALUE436437 006C 3A 00 00     E      LDA TMZERO438 006F FE 02   CPI 2          ELSE IF TMZERO &lt; 2, THEN439 0071 DA 84 00     C      JC OKFIR       GOTO OKFIR440 0074 FE 03   CPI 3          ELSE IF TMZERO &gt;= 3, THEN441 0076 D2 E8 01     C      JNC CKLATE     GOTO CKLATE442              REPT 8         ELSE443              XTHL           DELAY ONE DEGREE444              ENDM453 0081 C3 84 00     C      JMP OKFIR      GOTO OKFIR454                             END ENDIF__________________________________________________________________________