Difference between revisions of "LDR PID controller (LDRPID)"

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''Special thanks to [http://www.nefariousmotorsports.com/forum/index.php/topic,555.0title,.html phila_dot] for translating this section.''
 
''Special thanks to [http://www.nefariousmotorsports.com/forum/index.php/topic,555.0title,.html phila_dot] for translating this section.''
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[[Category:Motronic]]

Revision as of 06:53, 2 June 2011

This is a translation from the Funktionsrahmen

LDRPID abbreviations

Parameter Source-X Source-Y Type Designation
CWLDIMX FW Code word for application procedures KFLDIMX / KFLDIOPU
FTLDIA FW Factor for Debounce adaptation release
FTLDIAP FW Factor for Debounce positive fast tracking
KFLDIMX NMOT_W PLSOLR_W KF Map LDR I-control limit
KFLDIOPU NMOT PU KF Correction of TV values by the amount influence
KFLDIWL TMST IMLATM KF Correction LDR I-limitation in the warm-up
KFLDRL NMOT_W LDTVR_W KF KF for linearizing boost pressure = f (TV)
KFLDRQ0 NMOT LDE KF LDR-control parameters Q0
KFLDRQ1 NMOT LDE KF LDR controller parameter Q1 (Integrator coefficient)
KFLDRQ2 NMOT LDE KF Map LDR controller parameter Q2
KFRBGOF NGFIL NMOT KF Offset for I-component limit LDRPID
LDAMN FW Minimum limitation of the adaptation LDR I-adaptation
LDDIAN FW Increment per program run for negative-tracking I-limit
LDDIAP FW Increment per program run for positive tracking I-limit
LDDIMNN NMOT_W KL Safety distance LDR I-controller limit negative
LDDIMXN NMOT_W KL Safety distance LDR I controller limitation
LDEIAO FW Upper deviation threshold for negative adjustment
LDEIAP FW Deviation threshold for positive adaptation I controller
LDEIAPS FW Deviation threshold for fast Positive-tracking
LDEIAU FW Deviation lower threshold for negative adjustment
LDHIA FW Hysteresis for LDR I-adaptation curve
LDIATA TANS KL Correction I-boundary LDR PID controller as a function of TANS
LDMXNN FW Limiting max tracking. LDR negative for controller adaptation
LDMXNP FW Limiting max tracking. LDR adaptation positive range change
LDRQ0S FW Controller parameters Q0 LDR-PID controller in stationary mode
LDRQ1ST NMOT KL Controller parameters Q1 PID controller in stationary mode (coefficient Integrations)
LDRVL FW Full load detection threshold LDR
NLDIAPU PU KL Speed threshold for adaptation I-limit
SLD04LDUB LDE SV (REF) Reference points distribution for boost control
SNG08LDUB NGFIL SV (REF) Reference points distribution of ngfil in LDR
SNM08LDUB NMOT SV (REF) Reference points distribution for boost control
SNM08LDUW NMOT_W SV (REF) Reference points distribution for boost control
SNM16LDUB NMOT SV (REF) Reference points distribution for boost control
SNM16LDUW NMOT_W SV (REF) Reference points distribution for boost control
SPL08LDUW PLSOLR_W SV Reference points distribution for boost control
SPS08LDUW PSSOL_W SV (REF) Reference points distribution for boost control
SPU08LDUB PU SV (REF) Reference points distribution for boost control
STA08LDUB TANS SV (REF) Reference points distribution for boost control
STLDIA1 FW Reference point 1 for LDR adaptation characteristic
STLDIA2 FW Reference point 2 for LDR adaptation characteristic
STLDIA3 FW Reference point 3 for LDR adaptation characteristic
STLDIA4 FW Reference point 4 for LDR adaptation characteristic
STV10LDSW LDTVR_W SV Reference points distribution for boost control
SY_TURBO SYS (REF) Turbocharger system constant
TLDIAN FW Debounce time for tracking I-negative adaptation
TLDIAPN NMOT KL Debounce time for tracking I-positive adaptation
TVLDMX FW Upper limit for duty cycle LDR
UMDYLDR FW Switching threshold dynamics LDR
Variable Source Type Designation
B_ADRLDRA PROKONAL EIN Boost adaptation values at delete of fault memory
B_LDDY LDRPID LOK Flag for dynamic operating condition LDR
B_LDIMXA LDRPID LOK Condition for adaptation limit value I portion LDR
B_LDIMXN LDRPID LOK Condition for negative correction ldimxr
B_LDIMXP LDRPID LOK Condition for positive correction ldimxr
B_LDR BBLDR EIN Flag for condition LDR active
B_LDVL LDRPID LOK Full load condition for LDR
B_PWF EIN Power fail condition
B_STLDW LDRPID LOK Condition Reference points LDR change adaptation
DFP_LDRA LDRPID DOK SG int error path no deviation boost
E_LDRA LDRUE EIN Error flag: boost pressure control error
IMLATM ATM EIN integr. Air mass flow from engine start to max value
IRBGOF_W LDRPID AUS Offset for I controller limitation LDRPID depending on speed gradient
LDE LDRPID AUS LDR-control error (set point - process value)
LDIMN_W LDRPID LOK Current value to the minimum value limit I component LDR
LDIMXA LDRPID LOK Adaptive correction of the LDR I controller maximum limit
LDIMXAK_W LDRPID AUS Current corrected limiting value I share LDR
LDIMXRK_W LDRPID LOK LDR I max. Limiting value (corrected reference value)
LDIMXR_W LDRPID LOK Current reference value for the maximum limit I component LDR
LDIMX_W LDRPID LOK Current value to the maximum limit I portion LDR
LDITV_W LDRPID LOK LDR, duty cycle of I-controller (word)
LDPTV LDRPID LOK LDR, duty cycle of the P-controller
LDRDTV LDRPID LOK LDR duty cycle of the D controller
LDRKD_W LDRPID LOK LDR-control parameters for D-term
LDRKI_W LDRPID LOK LDR-control parameters for I-share
LDRKP_W LDRPID LOK LDR-control parameters for P component
LDTV LDRPID AUS LDR duty cycle
LDTVR_W LDRPID LOK LDR duty cycle from the controller
NGFIL BGNG EIN filtered speed gradient
NMOT BGNMOT EIN Motor speed
PLGRUS_W BGPLGU EIN Base boost pressure set point
PLSOL FUEDK EIN Reference boost pressure
PLSOLR_W LDRPID LOK Relative target boost pressure LDR
PLSOL_W FUEDK EIN Reference boost pressure
PU GGDSAS EIN Ambient pressure
PVDKDS GGDSAS EIN Pressure upstream of throttle valve pressure sensor
RLMAX_W LDRUE EIN maximum possible load, for Turbo
RLSOL_W MDFUE EIN Nominal charge
STLDIA LDRPID LOK Current Reference point for LDR adaptation
TMST GGTFM EIN Engine starting temperature

LDRPID Functions

With active LD regulation (B_ldr) is used to calculate deviation charging the difference between plsol and pvdkds (Pressure at throttle) is formed, while with inactive LD-control lde is set to 0.

PID controller: This control scheme uses a PID controller of type 3PR2 (3 parameters-controller with 2 output parameters to be optimized) with adaptive semi-pilot I component. The I-component is in the form of a MIN / MAX limitation within an applicable tolerance limits of the adaptive after-run steady TV-requirements conducted. To use the entire TV range (very different slopes), it is necessary to control SW-side to linearize so that results from the perspective of the regulator is a linear behavior. This is achieved with the map KFLDRL, which is a control of duty cycle incoming opposed to an applied Nonlinearity transformed so that from control point of view, the controlled system appears linear.

Control algorithms:

P-portion: ( LDRQ0DY ( or LDRQ0S ) - KFLDRQ2 ( or 0 ) ) * lde = ldptv
I-portion: lditv(i-1) + KFLDRQ1 ( or LDRQ1ST ) * lde(i-1) = lditv
D-portion: ( lde - lde(i-1) ) * KFLDRQ2 ( or 0 ) = ldrdtv

Operation: There are basically two different operating modes distinguished:

  1.  ! B_lddy: Quasi Stationary operation with PI control and the corresponding control parameters (relatively weak control intervention) Application of the controller parameters are on the engine test stand(dyno?) by a oscillation test according to Ziegler-Nichols.
  2. B_lddy: dynamic performance with PID controller and the corresponding control parameters (strong control intervention), the application Controller parameters are Einschwingversuch (Transient experiment?) by the Engine Laboratory(dyno?).

The distinction between these operating states via the control error, ie above a positive threshold deviation the dynamic control intervention and activated only at the change of sign of the deviation (actual value overshoots) withdrawn. The settling is done with the aim of not a oscillation, overshoot in the entire range in the quasi stationary mode. In this quasi-steady-state operation, the D component of the corresponding parameter setting signal is switched off to prevent unnecessary noise to avoid. In the dynamic operation, with the help of the highly engaging P component to achieve a minimum settling time.

The control is strong up to perform and improve the transient response further, the I-component with an adaptive Limit provided. This limitation is a function of n, plsol, pu, tans and additively superimposed 5 Range Adaptation. This limitation prevents reliable I-controller-related overshoot conditions, as a result of greater integration of an applicable Safety distance LDDIMXN above or below the small LDDIMN stationary integration needs to be prevented. The structure the limitation is interpreted as follows:

Means-tested tracking and adaptation:

  1. negative tracking
    1. Since the quasi-steady state is under full load (B_ldvl) at B_ldr the end of the debounce TLDIAN the current limit value ldimxr with the step size LDIAN as long as to smaller TV-values through corrections to the corrected value the current I-Share (lditv) is achieved.
    2. If in the dynamic operation under full load, an overshoot greater than LDEIAU for more than TLDIAN found so also reduced ldimxr.
  2. positive follow-up
    • If the current limit value is too low order to correct fully (deviation> LDEIAP (-20 mbar)), lditv (> = ldimxr + ldimxak), closed-loop B_ldr), the stop is after a nmot dependent debounce TLDIAPN with the Increment LDDIAP per program run, the current limit value ldimxr as long as corrected to higher values out to The current need for integration is now covered and the predetermined safety margin of the integrator to limit value is maintained. The engine speed must always be above NLDIAPU. In addition to the o.g. Conditions, the only slight deviation (lde <LDEIAPS, for example 60 mbar), then it will be that FTLDIAP reduced debounce previously tracked positive.
  3. Adaptation read
    • When you enter B_ldr (lditv> 0) or reference points change the adaptation range is read, and the change between is limited to the current adaptive value and the current adjustment value to LDMXNN or LDMXPN. This discontinuity in the driving behavior can be prevented.
  4. Leave adaptation
    • The storing of this adjustment value (Leave adaptation) is only after the debounce time TLDIAPN event of a recognized Full load (B_ldvl) and above a speed threshold (NLDIAPU).

LDRPID Application Notes

Interpretation:

  1. Linearization map KFLDRL specify:
    • On the dyno the course of the boost pressure is pvdkds be determined as a function of duty cycle. This should be fully open, the duty cycle controlled DK (CWMDAPP) is significantly above the normal max. Boost pressure beyond will be moved (if possible up to 300 mbar over the max. turbocharging pressure) to determine the course as possible. This approach is starting at 1500 rpm in 500 rpm increments to Nmax performed. The necessary linearization values are below graphically at any speed (or calculated) determined as follows: In a chart pvdkds = f (ldtvm) is by the first measuring point (0%) and by the last measuring point (max. 95%) is a straight lay. Thereafter, for example starting at 10% TV of the corresponding pressure value of the line is determined and the value of this pressure belonging to ldtvm value of the curve. Ldtvm This value is now entered in each of the map KFLDRL at the corresponding reference point (here, 10%). At the latest when it reaches 95% TV (= LDTVMX) must be ensured that the incoming duty cycle is equal to the is outgoing. Application target the widest possible linearization of the controlled system from the perspective of the regulator.
  2. LDRQ0DY by the process of so-called manipulated variable set, ie in the lowest speed within B_ldr is under Full load, the control variable (TV) amount to just a short time equal to 100%. Including the project-specific boundary condition maximum deviation Emax (mean VI value - medium base boost pressure value) is calculated as follows to LDRQ0DY:
    LDRQ0DY = 100% / emax (% TV /100hPa)
  3. KFLDRQ2: at n <2500 rpm = 0, for n> 2500 in range of medium-sized deviations (lde) stepwise to max. 0.6 (max. 0.9) * LDRQ0DY increase, at n> 2500 rpm and lde <100 hPa and LDE> approximately 500 hPa KFLDRQ2 sliding to 0 to reduce if benefits result. For problems with overshooting - only by the motor / ATL due (check by Einschwingversuch with pure control) - should be tried by large KFLDRQ2 values related with slightly larger LDRQ0DY values to hold.
  4. Stationary control parameters
    1. LDRQ0S after a oscillation test with P controller by the Ziegler-Nichols on the engine test bench: VL-operating points (possibly with overboost) in Speed range of the maximum torque of the motor (nMdmax -100 +300 /min ) with PI controller (initially weak control of intervention parameters adjusted!) approach to control deviation is zero. Then change by LDRQ1ST = 0 to P-control and as long as LDRQ0S increase until significant overshooting of the controlled variable occurs. This controlled variable suitably keeps a record, of the cycle time (Tkrit.) to read an oscillation (clearly recognizable sinusoidal curve necessary). With the two readings is crit. and LDRQ0S (krit.) parameters LDRQ0S and LDRSTQ1 can now be determined as follows: Note: UMDYLDR for this test to the set maximum value!
      LDRQ0S = 0.4 * LDRQ0S (kit.)
    2. LDRSTQ1 = 0.5 * LDRQ0S(krit.) * T0 / Tkrit. ; T0 = sampling time (i.d.R. = 0.05 s) for all parameters over n i.d.R. same values apply. The determined values below 3 can (and should) be reduced if benefits are reflected in driving behavior. An increase is not permitted for reasons of stability!
  5. I-set limit:
    • KFLDIMX: describe the steady pulse duty factor.
    • KFLDIOPU: duty cycle correction needed as a function of height (pu) described. LDIATA: need for correction as a function of tans set
Adaptation of I-Limit
Recognition LDR full load applied so that about 2% is detected before the actual pedal stop B_ldvl.
LDEIAU: approximately  -100 mbar
LDAMN:                 -15...-20 %
LDEIAO:                20...30 mbar
LDEIAP:  approximately -20 mbar
LDEIAPS: approximately 60 mbar
TLDIAN:  approximately 0.3 s
TLDIAPN: approximately 1.5 * T95-time in each case
FTLDIAP: approximately 0.1...0.2
FTLDIA:  approximately 0.5...1
NLDIAPU: The response speed (Highest VL-pressure regulated) as f (pu) + approx 250/min
Caution: Make sure that lowest learning cell is described in the height, otherwise when starting from low
          Speed of adaptation initial value of the lowest learning cell (=0%) were removed and the cells overlying the
          Change limit corrected (wrong) are overwritten!
STLDIA 1> NLDIAPU (Max)
LDMXNN: about 5%
LDMXNP: about 5%
  1. UMDYLDR: about 5% of the maximum reference value
  2. KFLDRQ1: Set so that when the transient due to load jumps from medium load to full load the I component end of the transient short-term just the current limit value ldimx affected (at all speeds!). This Appl.-step LDDIMXN to max. 2 to 3% amount!
  3. LDDIMXN: about 15% below NLDIAPU (highest speed) and about 3% above this speed (the same safety distance around fully to control from)
  4. LDDIMNN: apply in the case of transitional problems in light dynamic about 5%, otherwise use the maximum value to function lay dead.

Special thanks to phila_dot for translating this section.

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