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Am J Physiol Heart Circ Physiol 273: H2044-H2061, 1997;
0363-6135/97 $5.00
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Vol. 273, Issue 4, H2044-H2061, October 1997

MODELING IN PHYSIOLOGY
Left ventricular pressure response to small-amplitude, sinusoidal volume changes in isolated rabbit heart

Kenneth B. Campbell1,2, Yiming Wu1, Robert D. Kirkpatrick1, and Bryan K. Slinker1

1 Departments of Veterinary and Comparative Anatomy, Pharmacology, and Physiology and 2 Department of Biological Systems Engineering, Washington State University, Pullman, Washington 99164-6520

    ABSTRACT
Top
Abstract
Introduction
Methods
Conclusions
Appendix
References

The objective was to determine the dynamics of contractile processes from pressure responses to small-amplitude, sinusoidal volume changes in the left ventricle of the beating heart. Hearts were isolated from 14 anesthetized rabbits and paced at 1 beats/s. Volume was perturbed sinusoidally at four frequencies ( f ) (25, 50, 76.9, and 100 Hz) and five amplitudes (0.50, 0.75, 1.00, 1.25, and 1.50% of baseline volume). A prominent component of the pressure response occurred at the f of perturbation [in-frequency response, &Dgr;P<SUB><IT>f</IT></SUB> (t)]. A model, based on cross-bridge mechanisms and containing both pre- and postpower stroke states, was constructed to interpret &Dgr;P<SUB><IT>f</IT></SUB> (t). Model predictions were that &Dgr;P<SUB><IT>f</IT></SUB> (t) consisted of two parts: a part with an amplitude rising and falling in proportion to the pressure around that which &Dgr;P<SUB><IT>f</IT></SUB> (t) occurred [Pr(t)], and a part with an amplitude rising and falling in proportion to the derivative of Pr(t) with time. Statistical analysis revealed that both parts were significant. Additional model predictions concerning response amplitude and phase were also confirmed statistically. The model was further validated by fitting simultaneously to all &Dgr;P<SUB><IT>f</IT></SUB> (t) over the full range of f and Delta V in a given heart. Residual errors from fitting were small (R2 = 0.978) and were not systematically distributed. Elaborations of the model to include noncontractile series elastance and distortion-dependent cross-bridge detachment did not improve the ability to represent the data. We concluded that the model could be used to identify cross-bridge rate constants in the whole heart from responses to 25- to 100-Hz sinusoidal volume perturbations.

cross-bridge model; cross-bridge detachment; cross-bridge power stroke; heart muscle

    INTRODUCTION
Top
Abstract
Introduction
Methods
Conclusions
Appendix
References

PRESSURE RESPONSES to controlled volume perturbation of the left ventricle (LV) of the beating heart have long been used to characterize ventricular mechanodynamics. These pressure responses have been elicited using a variety of volume perturbation protocols including 1) sustained constant-flow volume withdrawal over periods sufficient to achieve a given volume at a specified time in the cardiac cycle (29-31, 35); 2) rapid small-volume withdrawal at each of several times during the cardiac cycle (1, 13, 25, 26, 38); 3) small-volume withdrawal of varying amplitude and rate at the time of peak systolic pressure (4, 5, 9, 27); and 4) sinusoidal volume change over the entire time course of the cardiac cycle (32, 33). Analyses of the resultant data have related pressure to volume and flow. Conclusions from all these analyses point to an organ with complex mechanodynamics that varies with time over the course of the cardiac cycle. These analyses have emphasized global features such as chamber elastance, viscous resistance, and series elastance and have made only indirect associations between these global features and the underlying muscle properties responsible for them. Recently, there has been an effort to interpret LV pressure responses directly in terms of underlying muscle mechanisms (3, 5, 7, 27). The promise from these early studies is that by using carefully controlled small-amplitude perturbations and appropriate model-based analysis, detailed kinetic behavior of cardiac muscle may be elucidated from observations of pressure responses to volume changes in the whole heart.

In this study, we pursued that promise by using one of the original volume perturbation protocols: a continuous high-frequency, small-amplitude, sinusoidal volume change delivered over the entire cardiac cycle (32, 33). We chose this protocol not only because of the history of its previous use but also because it provides a means for identifying underlying contractile behavior from observations in the whole heart; these observations extend over the entire cycle period and are not confined to a very brief 20-ms interval at the time of peak isovolumic systole as in our previous studies (5, 27, 28). Furthermore, we employed a cross-bridge model with pre- and postpower stroke elastance states to describe, predict, and explain the observed pressure responses. We concluded that these experimental and analytic techniques could be used to extract information about underlying cross-bridge mechanisms from observations made in the whole heart.

Glossary

A1 Amplitude scaling factor for pressure response component that varies proportionately with Pr(t)
A2 Amplitude scaling factor for pressure response component that varies proportionately with time drivative of &Pdot;r(t)
AIC Aikake Information Criterion
Ap Amplitude of dynamic passive component
b, d Rate constants governing formation and dissolution of prepower stroke state
Bn Amplitude of the nth harmonic of Delta Pd(t)
 Delta P(t) Pressure response to volume perturbation
 Delta Pd(t) Depressive component of pressure response
 Delta Pf(t) In-frequency component of pressure response
 Delta Pfa(t) Active part of in-frequency response
 Delta Pp(t) Dynamic passive component of pressure response
 Delta V Measured amplitude of volume perturbation
 Delta V(t) Time-varying volume perturbation
 Delta Vc Computer-commanded amplitude of volume perturbation
Ee0(t) Elastance of pressure generators in the prepower stroke state
Eep(t) Elastance of pressure generators in the postpower stroke state
ESE Elastance of series-coupled noncontractile element
ci regression coefficient
 epsilon Elastance of a single generator
f Frequency of volume perturbation
g Rate constant governing cross-bridge detachment
h Rate constant governing power stroke
K Number of parameters
 Delta lm/2 Change in half-mass wall circumference
N Number of sampled data points
Ne0(t) Number of pressure generators in the prepower stroke state
Nep(t) Number of pressure generators in the postpower stroke state
P(t) Pressure of perturbed beat
Piso(t) Pressure of isovolumic (unperturbed) beat
Pr(t) Pressure around which Delta Pf (t) occurred
Q10 Relative rate of change with a 10°C increase in temperature
 phi1 Phase of pressure response component that varies proportionately with Pr(t)
 phi2 Phase of pressure response component that varies proportionately with &Pdot;r(t)
 phip Phase of dynamic passive component
RSS Residual Sum of Squares
SC Schwartz Criterion
T Period of a heartbeat
 theta n Phase of the nth harmonic of Delta Pd(t)
VBL Baseline volume
VW Wall volume
 sigma Wall stress
 omega Angular frequency
X0 Average isovolumic distortion of postpower stroke generators
Xe0(t) Average distortion of prepower stroke generators
Xep(t) Average distortion of postpower stroke generators
Zep Total distortion among all ep generators

    EXPERIMENTAL METHODS AND PROCEDURES
Top
Abstract
Introduction
Methods
Conclusions
Appendix
References

Experimental Preparation

Hearts were isolated from 14 adult male rabbits (avg wt = 3.1 kg). Procedures for isolating the heart and attaching it to a volume-servo device have been described in detail elsewhere (7, 19). Briefly, the brachiocephalic artery was cannulated, and perfusion was begun with oxygenated relaxing solution (in mM: 121.4 Na+, 35.0 K+, 137.4 Cl-, 0.1 Ca2+, 1.1 Mg2+, 21.0 HCO<SUP>−</SUP><SUB>3</SUB>, 0.36 PO<SUP>3−</SUP><SUB>4</SUB>, and 11.1 glucose and 2.5 U/l insulin) to stop the heart before it was isolated from the animal. The perfusate was oxygenated by vigorously bubbling with 95% O2-5% CO2.

The heart was transferred to a perfusion support system consisting of a gas-exchange chamber, a roller pump, a constant-pressure chamber, and an environmental chamber. The heart was placed within an environmental chamber where the coronary arteries were perfused at 90 mmHg. Temperature was kept constant at 30°C. The heart was submerged in perfusate at all times by allowing the coronary effluent to accumulate in the environmental chamber until it reached the chamber overflow at the level of the base of the heart. The perfusate was not recirculated.

A thin latex balloon, secured to the piston cylinder of a volume-servo system, was drawn into the LV chamber such that its tip was anchored through a puncture in the apex, which also served as a vent for any fluids between the balloon and chamber wall. A draw-string suture in the mitral annulus was tightened around the obturator of a piston-cylinder device, which secured the balloon in the LV chamber. The balloon was filled with degassed distilled water until passive chamber pressure reached 10 mmHg. Balloons were sized to fill the LV without excessive folding and without developing pressure at the volumes encountered in these ventricles. Thus balloons did not contribute to measured pressure.

The perfusing solution was changed from the relaxing solution to one that allowed spontaneous beating (in mM: 148.4 Na+, 7.4 K+, 139.1 Cl-, 1.24 Ca2+, 1.1 Mg2+, 21.0 HCO<SUP>−</SUP><SUB>3</SUB>, 0.36 PO<SUP>3−</SUP><SUB>4</SUB>, and 11.1 glucose and 2.5 U/l insulin). The heart, suspended in the spent perfusate, was paced at 1 Hz with field stimulation using 5-ms pulses of 15 mV and 250 mA from 5 cm × 5 cm copper plates placed 4.5-cm apart on either side of the heart.

The volume-servo system consisted of a linear motor, a piston-cylinder device, and a linear variable differential transformer (LVDT, model 0294-0000, Trans-Tek). The piston-cylinder device was a modified 5-ml glass syringe (East Rutherford Syringes) with two side ports. One side port allowed calibrated infusion of fluid into the LV balloon to establish a baseline volume (VBL). The second port was used to introduce a 5-Fr catheter-tip pressure transducer (Millar, Houston, TX) into the balloon. The piston was driven by the armature shaft of the linear motor. Motions of the piston produced LV volume changes around VBL at a resolution of 0.001 ml. Both the pressure measurement system and the LVDT system had frequency responses of 1 kHz.

Motion of the motor armature, and consequently piston motion, was controlled to achieve specified changes in LV volume by feeding back the position signal from the LVDT transducer, comparing it with a reference position signal from a supervisory-control computer, and passing the difference through an analog proportional-integral-derivative compensator. Output from the compensator was used to drive a high-current amplifier, which delivered electrical current to the motor, causing piston position to match the volume command.

The supervisory-control computer controlled experimental protocols according to programmed instructions and also acquired data for later analysis. Pressure and volume signals were amplified to make maximal use of the 12-bit range of an analog-to-digital converter and were acquired at a 2-kHz sampling rate.

Experimental use of animals was approved by the Animal Care and Use Committee at Washington State University. The investigation conforms with the Guide for the Care and Use of Laboratory Animals published by the National Institutes of Health (NIH publication No. 85-23, Revised 1985).

Protocols

A single-beat Frank-Starling protocol (7) was conducted to establish VBL for each heart. VBL was chosen as the volume equal to 80% of the volume at which maximum pressure was developed. This protocol was also used to establish the passive pressure-volume relationship. A monoexponential equation was fit to points over the range of end-diastolic pressure and volume values generated in this protocol. Thus the contribution to pressure by parallel passive structures at any volume was estimated and removed from all ensuing data records in order to allow us to focus on just active contractile properties.

After VBL was established, a high-frequency volume perturbation protocol was conducted as follows. Twenty pairs of data records consisting of pressure and volume signals were taken. One record in a pair contained a single volume-perturbed beat, and the other record contained an unperturbed beat that served as a reference. Volume perturbation was administered only on a selected single beat. On the perturbed beat, the linear motor was commanded to deliver a sinusoidal volume change at one of four frequencies (100, 76.9, 50, or 25 Hz, corresponding to periods of 10, 13, 20, or 40 ms) and one of five amplitudes (0.5, 0.75, 1.0, 1.25, or 1.5% of VBL). Repeated records of perturbed beats were taken until all combinations of frequencies and amplitudes (20 perturbed beats) were recorded. Pressure responses to the volume perturbation were then analyzed.

Because the volume-servo system was underdamped, the actual volume perturbation did not exactly equal the commanded sinusoid from the supervisory-control computer. The frequency ( f ) of actual and commanded signals was the same, but there were differences between actual and commanded amplitudes (Delta V and Delta Vc, respectively), and there was 1-2 ms delay in the actual signal relative to the commanded signal. Consequently for some analyses (see below), each of the measured volume perturbation signals was fitted with the analytic function
&Dgr;V(<IT>t</IT>) = &Dgr;V sin (2&pgr;<IT>ft</IT> + ϕ) (1)
where phi was a phase relative to the recorded time window. Equation 1 fitted all measured Delta V(t) with a correlation coefficient (R2) > 0.99 and was thus judged to be an adequate representation of the actual perturbation signal for specific analyses. The underdamped character of the volume-servo system produced an actual Delta V that, for a given Delta Vc, increased with frequency over the 25- to 100-Hz frequency range with the result that the actual Delta V at 100 Hz was 145% of that at 25 Hz. Thus Delta V from the fit to the measured signal was used rather than the commanded Delta Vc in all data analyses.

After the high-frequency volume perturbation protocol, a second single-beat Frank-Starling protocol was conducted to generate a Frank-Starling curve that could be compared with the one collected previously. This allowed detection of any deterioration of the preparation during the course of an experiment. No detectable deterioration occurred.

    PRESSURE RESPONSE

Peak isovolumic pressure generated by these 14 hearts (averaged over all 280 observations) was 120.2 ± 13.6 (SD) mmHg at an average VBL of 2.11 ± 0.09 ml. The average LV weight, including the septum plus LV free wall, was 5.96 ± 0.54 g.

The pressure response [Delta P(t)] to Delta V(t) was defined as the difference between active pressure of the reference isovolumic beat [Piso(t)], i.e., the pressure that would have developed had no volume perturbation been administered, and active pressure of the perturbed beat, P(t)
&Dgr;P(<IT>t</IT>) = P(<IT>t</IT>) − P<SUB>iso</SUB>(<IT>t</IT>) (2)
Representative Piso(t), P(t), and Delta P(t) are shown in Fig. 1 (f = 50 Hz, Delta Vc = 1% VBL). All responses [Delta P(t)] contained two components: a depressive response, Delta Pd(t) [called "depressive" because it represented a sustained decrease in pressure below Piso(t) that was not at the perturbation frequency] and an in-frequency response [&Dgr;P<SUB><IT>f</IT></SUB>(t)] (that part of the response at the perturbation frequency). Thus
&Dgr;P(<IT>t</IT>) = &Dgr;P<SUB>d</SUB>(<IT>t</IT>) + &Dgr;P<SUB><IT>f</IT></SUB>(<IT>t</IT>) (3)
The Delta Pd(t) was extracted from Delta P(t) by fitting a curve to Delta P(t) that did not contain frequency content of the perturbation frequency. Delta Pd(t) was taken as the sum of the first 10 harmonics in the Fourier series
&Dgr;P<SUB>d</SUB>(<IT>t</IT>) = <LIM><OP>∑</OP><LL><IT>n</IT>=1</LL><UL>10</UL></LIM> <IT>B</IT><SUB><IT>n</IT></SUB> sin <FENCE><IT>n</IT> <FR><NU>2&pgr;</NU><DE><IT>T</IT></DE></FR> + &thgr;<SUB><IT>n</IT></SUB></FENCE> (4)
where n is the harmonic number, Bn and theta n are harmonic amplitude and phase, respectively, of n, and T is the heart period. Because the shortest heart period used in these studies was 1 s, the 10th harmonic (10 Hz) was well below 25 Hz, the lowest frequency used for volume perturbation. The amplitude and phase parameters for the ith harmonic (Bi and &thgr;<SUB><IT>i</IT></SUB>) had no particular significance other than to give a Delta Pd(t) waveshape, identifiable within Delta P(t), that did not include components of the in-frequency response. Once Delta Pd(t) was identified by fitting with Eq. 4, it was subtracted from Delta P(t) to yield &Dgr;P<SUB><IT>f</IT></SUB> (t). Subtraction of Delta Pd(t) from Piso(t) generated a signal representing the pressure around which &Dgr;P<SUB><IT>f</IT></SUB> (t) took place [Pr(t)]. Pr(t), with corresponding Delta P(t), Delta Pd(t), and &Dgr;P<SUB><IT>f</IT></SUB> (t), is shown in Fig. 1.


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Fig. 1.   Method of determining pressure response [volume perturbation = 50 Hz, 1% baseline volume (VBL)]. A: 2 left panels: Piso(t), pressure of an isovolumic beat in which no volume perturbation was applied; P(t), pressure of a beat that received volume perturbation. Middle panel: Delta P(t), pressure response to volume perturbation [= P(t- Piso(t)]. Right panel: Delta Pd(t), depressive component of Delta P(t) obtained by low-pass filtering Delta P(t). Bottom panel: &Dgr;P<SUB><IT>f</IT></SUB> (t), in-frequency component of Delta P(t) [=Delta P(t- Delta Pd(t)]. B: pressure around which in-frequency response occurred [Pr(t)] was obtained by subtracting Delta Pd(t) from Piso(t). Vertical scale is in mmHg, horizontal scale is in s.

This report concerns just &Dgr;P<SUB><IT>f</IT></SUB> (t); the Delta Pd(t) is the subject of another report (unpublished observations). Twelve of twenty &Dgr;P<SUB><IT>f</IT></SUB> (t) responses obtained in one heart are shown in Fig. 2. &Dgr;P<SUB><IT>f</IT></SUB> (t) rose and fell during the course of the heartbeat but also contained a small contribution that was present during diastolic periods when there was no active contraction. This small component was assumed to be due to dynamic features of parallel passive properties that were not included in the static passive pressure-volume relationship, which had already been subtracted from the response. Furthermore, these passive dynamic properties were assumed to be expressed continuously throughout the period of the heartbeat and, for a given Delta V(t) sinusoid, they were represented as
&Dgr;P<SUB>p</SUB>(<IT>t</IT>) = <IT>A</IT><SUB>p</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>p</SUB>) (5)
This passive dynamic response was subtracted from the response signal using data-fitting procedures described below. The great majority of &Dgr;P<SUB><IT>f</IT></SUB>(t) waxed and waned as pressure rose and fell and was considered to be an expression of active processes. Thus
&Dgr;P<SUB><IT>fa</IT></SUB>(<IT>t</IT>) = &Dgr;P<SUB><IT>f</IT></SUB>(<IT>t</IT>) − &Dgr;P<SUB>p</SUB>(<IT>t</IT>) (6)
where &Dgr;P<SUB><IT>fa</IT></SUB>(t) was the contribution of active process to &Dgr;P<SUB><IT>f</IT></SUB> (t).


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Fig. 2.   &Dgr;P<SUB><IT>f</IT></SUB> (t) over single heartbeat for 12 of 20 responses in one heart, showing extremes and midrange of responses to various amplitudes and frequencies of Delta V(t). Note growth in amplitude of response with both amplitude and frequency of Delta V(t). A: 0.5%; B: 1.0%; C: 1.5%.

It is clear from Fig. 1 that, in accordance with results from several studies (1, 13, 25, 29, 32, 38), &Dgr;P<SUB><IT>fa</IT></SUB>(t) waxed and waned during the heart period as Pr(t) rose and fell. One objective of the current work was to predict from model considerations whether other time-varying components were contained within &Dgr;P<SUB><IT>fa</IT></SUB>(t) and, then, to test these predictions.

    MODEL DESCRIPTION

A model for describing and predicting the active part of the pressure response [&Dgr;P<SUB><IT>fa</IT></SUB>(t)] was constructed on the assumption that elements responsible for force generation in cardiac muscle (i.e., cross-bridges between thick and thin myofilaments) were also responsible for pressure generation in the LV chamber. Furthermore, it was assumed that there was a straightforward linear transformation between force-length relationships in the wall of the heart and pressure-volume relationships in the LV chamber. Acceptability of the linear transformation assumption requires small-amplitude perturbations and homogenous myocardium. Criteria for satisfying the small-amplitude requirement are detailed in the APPENDIX. Evidence that the homogenous myocardium requirement is satisfied is given in the findings relative to the unimportance of noncontractile series elasticity in these hearts (see MODEL VALIDATION). However, a strong reason for employing the linear transformation assumption is the success that has been achieved with its application in earlier studies (3, 5, 6, 27).

It was further assumed that during a heartbeat mechanodynamics were from two sources: 1) dynamics of activation as activator Ca2+ comes and goes and numbers of force-bearing cross-bridges rise and fall, and 2) dynamics of cross-bridge cycling as myosin heads cyclically attach to and detach from the actin binding site. In accordance with an earlier hypothesis (6), we argue that the only dynamics expressed within the brief cycle period of frequencies >= 25 Hz were those associated with steps in the cross-bridge cycle and that the dynamics of activation were too slow to contribute to changes within these brief time periods. Such separation of time scales in the study of muscle dynamics is in accordance with analyses conducted by Kawai and co-workers (17, 24, 39) and in accordance with our recent demonstration that cooperativity between force-bearing cross-bridges and activation can cause activation to be slow relative to cross-bridge dynamics (2).

We refer to cross-bridges as force generators. Generators contributing to the pressure response were assumed to be in two states: 1) a state that possessed elastance but did not, under isometric (isovolumic) conditions, generate pressure (state e0), and 2) a state that both possessed elastance and also generated isometric (isovolumic) pressure (state ep). When we assume linear, independent, and parallel generators, the elastance associated with each state is the number of parallel generators in that state (N) times the elastance of a single generator (epsilon ). Assuming that all generators in states e0 and ep possess the same epsilon , we show the net elastance of all parallel generators in each of the two states as
<IT>E</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>) = &egr; ⋅ <IT>N</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>) (7)
<IT>E</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>) = &egr; ⋅ <IT>N</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>) (8)
where, because of our linear transformation assumption, Ee0(t) and Eep(t) may be taken as volumetric elastances (with units of mmHg/ml).

Generators are in continual transition as they progress from one state to another in the cross-bridge cycle (Fig. 3). We assumed that state e0 preceded state ep. Furthermore, transitions into, out of, and between states e0 and ep were assumed to be governed by rate constants b, d, g, and h. State 0 in Fig. 3 is without elastance and is a precursor to state e0; state 00 is also without elastance and follows state ep. These nonelastance states represent all other states needed to complete a cross-bridge cycle. Given these relationships between states and assuming that there is no noncontractile series elastance (4), it is shown in the APPENDIX that Ee0(t) and Eep(t) may be calculated from Pr(t) and its first time derivative [&Pdot;r(t)] according to
<IT>E</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>) = <FR><NU><A><AC>P</AC><AC>˙</AC></A><SUB>r</SUB>(<IT>t</IT>) + <IT>g</IT>P<SUB>r</SUB>(<IT>t</IT>)</NU><DE><IT>hX</IT><SUB>0</SUB></DE></FR> (9)
and
<IT>E</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>) = <FR><NU>P<SUB>r</SUB>(<IT>t</IT>)</NU><DE><IT>X</IT><SUB>0</SUB></DE></FR> (10)
where X0 is a parameter representing average volumetric distortion among generators in state ep during isovolumic conditions. The transitional step between states e0 and ep, which is governed by h, is the cross-bridge power stroke, and this step is responsible for inducing X0 distortion in generators as they go through the power stroke to enter the ep state. The dissolution of the postpower stroke (ep) state, which is governed by g, is the cross-bridge detachment step.


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Fig. 3.   Schematic drawing of states in cross-bridge cycle. Ni is the number of generators in ith state. Generators in states e0 and ep possess elastance, whereas generators in states 0 and 00 do not. Generators possessing elastance may be distorted during a volume perturbation such that both contribute to pressure response. Under isovolumic conditions, generators enter state e0 without distortion and do not generate pressure. Transitions between states are governed by rate constants b, d, h, and g. Transition between state e0 and state ep is the power stroke and induces a baseline distortion in postpower stroke (ep) generators, which, as a result of their elastance, causes development of isovolumic pressure. Isovolumic pressure is modified during a volume perturbation by induced distortion in postpower stroke and prepower stroke states, ep and e0, respectively, and by whatever influence volume perturbation has on recruitment of generators into or out of cross-bridge cycle.

Because of their elastic nature, generators within each of these states are distorted during volume perturbation. The net volume-induced distortion is determined by the rate of volume change relative to the rates of formation and dissolution of the respective states. Differential equations for these volume-induced distortions [Delta Xe0(t) and Delta Xep(t) in states e0 and ep, respectively] are derived in the APPENDIX as
&Dgr;<IT><A><AC>X</AC><AC>˙</AC></A></IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>) = − <FENCE><FR><NU><IT><A><AC>E</AC><AC>˙</AC></A></IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>)</NU><DE><IT>E</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>)</DE></FR> + <IT>h</IT> + <IT>d</IT></FENCE> &Dgr;<IT>X</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>) + &Dgr;<A><AC>V</AC><AC>˙</AC></A>(<IT>t</IT>) (11)
&Dgr;<IT><A><AC>X</AC><AC>˙</AC></A></IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>) = − <FENCE><FR><NU><IT><A><AC>E</AC><AC>˙</AC></A></IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>)</NU><DE><IT>E</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>)</DE></FR> + <IT>g</IT></FENCE> &Dgr;<IT>X</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>) + &Dgr;<A><AC>V</AC><AC>˙</AC></A>(<IT>t</IT>) (12)
A dot over a variable indicates its first time derivative. In words, Eqs. 11 and 12 state that the time rate of change of generator distortion is negatively related to distortion itself and is positively related to the first time derivative of volume. Thus volume-induced distortion is driven directly by flow (velocity) and dies away at a rate proportional to the distortion.

Given these relationships, the model equation predicting the active part of the in-frequency pressure response [Delta &Pcirc;fa(t)] is
&Dgr;<A><AC>P</AC><AC>ˆ</AC></A><SUB><IT>fa</IT></SUB>(<IT>t</IT>) = <IT>E</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>)&Dgr;<IT>X</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>) + <IT>E<SUB>ep</SUB></IT>(<IT>t</IT>)&Dgr;<IT>X</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>) (13)
where the "hat" in Delta &Pcirc;fa(t) indicates that the quantity is model predicted.

Equations 9-13 constitute a 2-state, 4-parameter model. In this model, Delta V(t) is the input [although distortion is driven directly by Delta V(t)]; Ee0(t), Eep(t), and their time derivatives combine to form time-varying parameters; Delta Xe0(t) and Delta Xep(t) are state variables; and Delta &Pcirc;fa(t)is the output variable. Equations 11 and 12 are a set of linear, uncoupled, first-order, time-varying differential equations.

    MODEL PREDICTIONS

Two Dynamic Components of In-Frequency Response

In-frequency response consists of two dynamic components: 1) a component with an amplitude varying with Pr(t) and 2) a component with an amplitude varying with the time derivative of Pr(t). The model output equation Eq. 13 can be rearranged by substituting elastance Eqs. 9 and 10 into Eq. 13 to create an alternative formulation.
&Dgr;<A><AC>P</AC><AC>ˆ</AC></A><SUB><IT>fa</IT></SUB>(<IT>t</IT>) = P<SUB>r</SUB>(<IT>t</IT>) <FENCE><FR><NU>1</NU><DE><IT>X</IT><SUB>0</SUB></DE></FR></FENCE><FENCE><FR><NU><IT>g</IT></NU><DE><IT>h</IT></DE></FR> &Dgr;<IT>X</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>) + &Dgr;<IT>X</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>)</FENCE>
+ <A><AC>P</AC><AC>˙</AC></A><SUB>r</SUB>(<IT>t</IT>) <FENCE><FR><NU>1</NU><DE><IT>hX</IT><SUB>0</SUB></DE></FR></FENCE> &Dgr;<IT>X</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>) (14)

The first term on the right-hand side of Eq. 14 is a response component with an amplitude varying proportionately with Pr(t), and the second term on the right-hand side is a component with an amplitude varying proportionately with &Pdot;r(t). This development clearly identifies the contribution of the prepower stroke, e0 state as the sole source of the dynamic response component with an amplitude rising and falling in proportion to the derivative of the pressure around which the response is occurring.

To determine the relative roles of these two components, an approximate sinusoidal solution of the model equations Eqs. 11 and 12 was developed as follows. When we ignore the influence of the time-varying part of the coefficients in Eqs. 11 and 12, a steady-state solution of these equations for Delta Xe0(t) and Delta Xep(t) when Delta V(t) is a volume sinusoid of frequency f results in an expression for the first and second terms on the right-hand side of Eq. 14 as
<FENCE><FR><NU>1</NU><DE><IT>X</IT><SUB>0</SUB></DE></FR></FENCE><FENCE><FR><NU><IT>g</IT></NU><DE><IT>h</IT></DE></FR> &Dgr;<IT>X</IT><SUB><IT>e0</IT></SUB>(<IT>t</IT>) + &Dgr;<IT>X</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>)</FENCE> = <IT>A</IT><SUB>1</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>1</SUB>)
<FENCE><FR><NU>1</NU><DE><IT>hX</IT><SUB>0</SUB></DE></FR></FENCE> &Dgr;<IT>X<SUB>e0</SUB></IT>(<IT>t</IT>) = <IT>A</IT><SUB>2</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>2</SUB>) (15)
Such that for a volume sinusoid of frequency f
&Dgr;<A><AC>P</AC><AC>ˆ</AC></A><SUB><IT>fa</IT></SUB>(<IT>t</IT>) = P<SUB>r</SUB>(<IT>t</IT>)[<IT>A</IT><SUB>1</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>1</SUB>)]
+ <A><AC>P</AC><AC>˙</AC></A><SUB>r</SUB>(<IT>t</IT>)[<IT>A</IT><SUB>2</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>2</SUB>)] (16)

The relative role of the &Pdot;r(t) component in the observed responses was determined by an incremental approach. Equations 6 and 16 were combined and fit to the observed &Dgr;P<SUB><IT>f</IT></SUB> (t) by first excluding the &Pdot;r(t) component
&Dgr;<A><AC>P</AC><AC>ˆ</AC></A><SUB><IT>f</IT>1</SUB>(<IT>t</IT>) = <IT>A</IT><SUB>p</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>p</SUB>)
+ P<SUB>r</SUB>(<IT>t</IT>)[<IT>A</IT><SUB>1</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>1</SUB>)] (17)
and then including the &Pdot;r(t) component
&Dgr;<A><AC>P</AC><AC>ˆ</AC></A><SUB><IT>f</IT>2</SUB>(<IT>t</IT>) = <IT>A</IT><SUB>p</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>p</SUB>)
+ P<SUB>r</SUB>(<IT>t</IT>)[<IT>A</IT><SUB>1</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>1</SUB>)]
+ <A><AC>P</AC><AC>˙</AC></A><SUB>r</SUB>(<IT>t</IT>)[<IT>A</IT><SUB>2</SUB> sin (2&pgr;<IT>ft</IT> + ϕ<SUB>2</SUB>)] (18)
Fitting of Eqs. 17 and 18 to &Dgr;P<SUB><IT>f</IT></SUB> (t) was by an heuristic search algorithm (Levenberg-Marquardt algorithm, Argonne National Laboratory) to minimize the residual sum of squares (RSS).

To test for degradation or improvement in the representation of &Dgr;P<SUB><IT>f</IT></SUB> (t) signal with the addition of the two additional parameters in Eq. 18 that relate to the &Pdot;r(t) component, the Aikake Information Criterion (AIC) and the Schwartz Criterion (SC) were calculated from fits with both Eqs. 17 and 18 according to Landaw and DiStefano (20) as
AIC = <IT>N</IT> ln (RSS) + 2<IT>K</IT>
SC = <IT>N</IT> ln (RSS) + <IT>K</IT> ln (<IT>N</IT>) (19)
where N is the number of sampled data points, and K is the number of parameters. Note that the first term on the right-hand side of Eq. 19 is a measure of how well the model fit the data, whereas the second term is a penalty function based on the number of model parameters. Therefore, increasing the number of parameters increases AIC and SC unless there is a more than compensating reduction in RSS. In considering two competing equations such as Eqs. 17 and 18, the better representation is the one with the smallest AIC and SC. To further determine whether significant reduction in the RSS occurred with Eq. 18 compared with Eq. 17, an incremental F-test was used (11).

When fit to &Dgr;P<SUB><IT>f</IT></SUB> (t) of each of the 280 data records obtained in these hearts (14 hearts times 20 records/heart), both Eq. 17, which did not include the &Pdot;r(t) component, and Eq. 18, which did include this component, fit &Dgr;P<SUB><IT>f</IT></SUB> (t) very well with median R2 of 0.980 and 0.981, respectively. The contribution of the &Pdot;r(t) component was quite small as judged by the fact that A2 was always two-orders of magnitude less than A1. However, despite this small contribution, the inclusion of the &Pdot;r(t) component in Eq. 18 consistently reduced the AIC (only one exception in 280 instances; median reduction: -0.78%; range: 0.02 to -10.1%) and SC (14 exceptions in 280 instances; median reduction: -0.63%; range: 0.09 to -9.93%), suggesting that the addition of the two parameters associated with the &Pdot;r(t) component improved the representation of the information in the &Dgr;P<SUB><IT>f</IT></SUB> (t) signals. Furthermore, of the 280-response records analyzed, the incremental F-test generated an F-statistic that was significant at the P < 0.01 level in all 280 instances. Thus, although making only a small contribution in accounting for the total variability in &Dgr;P<SUB><IT>f</IT></SUB> (t), the &Pdot;r(t) component contributed significantly to representing its information content and in reducing the RSS.

To summarize these results, the model predicted that there would be an in-frequency response component with an amplitude rising and falling in proportion to the pressure around which the response occurred [Pr(t)] and another component with an amplitude rising and falling in proportion to the derivative of the pressure around which the response occurred [&Pdot;r(t)]. Analysis of all the response data revealed that the response was dominated by the Pr(t) component, although a small but significant component existed with an amplitude of which was proportional to &Pdot;r(t). Given the very small contribution by the &Pdot;r(t) component, the model was further used to test the importance of including this term in validation procedures described below.

Amplitude Ratio and Phase of Response

Additional model predictions resulted from considering the nature of the response just around the time of peak Pr(t), when &Pdot;r(t) approximated zero. When transients are ignored and it is assumed that steady state had been achieved at this time, an argument can be made that during a short interval around the time of peak pressure, the e0 state does not contribute to the response and the model reduces to
&Dgr;<A><AC>P</AC><AC>ˆ</AC></A><SUB><IT>fa</IT></SUB>(<IT>t</IT>) = <IT>E</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>)&Dgr;<IT>X<SUB>ep</SUB></IT>(<IT>t</IT>)
&Dgr;<IT><A><AC>X</AC><AC>˙</AC></A></IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>) = −<IT>g</IT>&Dgr;<IT>X</IT><SUB><IT>ep</IT></SUB>(<IT>t</IT>) + &Dgr;<A><AC>V</AC><AC>˙</AC></A>(<IT>t</IT>) (20)
Input-output relationships between Delta Xep(t) and Delta V(t) for this reduced model may be derived as
<FR><NU>&Dgr;<IT>X</IT><SUB><IT>ep</IT></SUB>(&ohgr;)</NU><DE>&Dgr;V(&ohgr;)</DE></FR> = <FENCE><FR><NU>&Dgr;<IT>X</IT><SUB><IT>ep</IT></SUB>(&ohgr;)</NU><DE>&Dgr;V(&ohgr;)</DE></FR></FENCE><IT>e </IT><SUP><IT>j</IT>&thgr;(&ohgr;)</SUP>
<FENCE><FR><NU>&Dgr;<IT>X</IT><SUB><IT>ep</IT></SUB>(&ohgr;)</NU><DE>&Dgr;V(&ohgr;)</DE></FR></FENCE> = <FR><NU>&ohgr;</NU><DE><RAD><RCD>&ohgr;<SUP>2</SUP> + <IT>g</IT><SUP>2</SUP></RCD></RAD></DE></FR>
&thgr;(&ohgr;) = 90° − tan<SUP>−1</SUP> <FENCE><FR><NU>&ohgr;</NU><DE><IT>g</IT></DE></FR></FENCE> (21)
where omega  is angular frequency in radians and equals 2pi f, |&Dgr;<IT>X</IT><SUB>ep</SUB>(omega )/Delta V(omega )| is the magnitude of an input-output amplitude ratio equivalent to A1/Delta V from the previous sinusoidal fits, and theta (omega ) is the phase difference between output pressure response and input volume sinusoid.

Two predictions result from Eq. 21: 1) the amplitude ratio will increase with frequency up to some plateau, provided the frequencies examined are in the vicinity of the characteristic frequency, g. At frequencies either far below or far above g, the amplitude ratio will change only weakly with frequency. 2) The phase of &Dgr;P<SUB><IT>f</IT></SUB> (t) will lead the phase of Delta V(t) by as much as 90° at low frequencies, but this phase lead will decline and approach zero as frequencies increase above g.

To test these model predictions, the amplitude ratio, A1/Delta V, was evaluated for its dependence on f and Delta V. As noted above, A1/Delta V will change sharply with f over a frequency range around the characteristic frequency of the underlying process. Additionally, A1/Delta V is not expected to be dependent on the amplitude of the Delta V input. Any dependence of A1/Delta V on the amplitude of the input is an indication of nonlinear processes that are not part of the current model. Nonlinearities may also show up as dependence of A1/Delta V on product combinations of f and Delta V. Stepwise regression analysis was used for these determinations. Regression equations were formulated as
<FR><NU>&Dgr;<IT>A</IT><SUB>1</SUB></NU><DE>&Dgr;V</DE></FR> = <IT>c</IT><SUB>0</SUB> + <IT>c</IT><SUB>1</SUB> <IT>f</IT> + <IT>c</IT><SUB>2</SUB>&Dgr;V + <IT>c</IT><SUB>3–7</SUB> ( <IT>f</IT>, &Dgr;V) (22)
where the ci values are regression coefficients and (f,Delta V) represents one or more of four candidate interaction terms: f · (Delta V), root-mean-squared (rms) flow; f  2 · (Delta V), rms acceleration; Delta V2, squared rms volume amplitude; and (f · Delta V)2, squared rms flow amplitude. The regression procedure used dummy variables and effects coding to account for between-subjects differences, and the subject dummy variables were forced into the stepwise regression (11). A candidate predictor variable was considered significant only when the P value for its inclusion was <0.05.

The dependence of A1/Delta V on f at the various commanded Delta Vc for one heart is shown in Fig. 4. At all Delta Vc, A1/Delta V increased with f. Furthermore, at f equal to 25, 50, and 76.9 Hz, A1/Delta V had virtually no dependence on Delta Vc; there was an apparent small dependence on Delta Vc at 100 Hz. Regression analysis of pooled data from all hearts revealed that, of all potential predictor variables, there was a significant dependence on f and Delta V2; the simplest best regression equation (leaving out terms for between subjects variability) was
<FR><NU><IT>A</IT><SUB>1</SUB></NU><DE>&Dgr;V</DE></FR> = 2.42 + 0.0113<IT>f</IT> − 311&Dgr;V<SUP>2</SUP>
<IT>R</IT><SUP>2</SUP>(adjusted) = 0.87 (23)
No interaction terms were found to be significant in this regression. Of the two significant predictor variables, f was the more important variable. For example, at f = 50 Hz and Delta V = 1%, the term in Eq. 23 due to f adds 0.55 units to A1/Delta V, whereas the term due to Delta V2 subtracts only 0.03 units, an 18-fold difference in sensitivity of A1/Delta V on these variables. The three important outcomes of this regression analysis are 1) A1/Delta V increased with f in accordance with Delta V(t) acting as the effective driving function; 2) because of the strong dependence on f, the characteristic frequency of the dynamic processes responsible for the Pr(t) response component lies either within or not far distant from the 25- to 100-Hz frequency range; and 3) the very small dependence of the Pr(t) response component on Delta V indicated that nonlinearities were not a large part of the underlying processes.


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Fig. 4.   Amplitude ratio (A1/Delta V) of &Dgr;P<SUB><IT>f</IT></SUB> (t) component proportional to Pr(t) as a function of frequency (f) and commanded amplitude (Delta Vc) of perturbation. open circle , Delta Vc = 0.50% VBL; +, Delta Vc = 0.75% VBL; ×, Delta Vc = 1.00% VBL; * Delta Vc = 1.25% VBL; bullet , Delta Vc = 1.50% VBL. A1/Delta V increases with frequency and has very little dependence on Delta Vc, as predicted by model.

Predictions with regard to the phase lead were not analyzed exhaustively. Rather, single cycles, spanning the time of peak Pr(t) of response to 1% Delta Vc at each frequency, were examined. In these, the phase of &Dgr;P<SUB><IT>f</IT></SUB> (t) led that of Delta V(t) at 25 Hz by ~30-40°, and this phase lead decreased progressively to approach zero at 76.9 and 100 Hz.

To summarize these results, model predictions with regard to frequency dependence of input-output amplitude ratio and phase relations were confirmed. These indirect confirmations of the model suggested a more rigorous model validation test.

    MODEL VALIDATION

Ability to Fit the Data

Model validation was, in part, by evaluating how well the model fit the full time course of the pressure response over an entire cardiac cycle. Model fitting was by the following procedure. Initial values of the four model parameters (g, h, d, and X0) and the two dynamic passive pressure parameters (Ap and phip) were assigned. Derivatives of measured Delta V(t) and Pr(t) were calculated using a five-point Lagrangian polynomial method. Measured Pr(t), the calculated derivatives, and the then-current parameter values were fed into the differential equations Eqs. 11 and 12, allowing these equations to be solved numerically by integrating with a fourth-order Runge-Kutta algorithm (integration step size = 0.0005 s) to obtain predictions of Delta Xe0(t) and Delta Xep(t). These were then used with measured Pr(t) and its derivative to compute a &Dgr;P<SUB><IT>fa</IT></SUB>(t) according to Eq. 13 and a Delta Pp(t) according to Eq. 5, which were then added to obtain a &Dgr;P<SUB><IT>f</IT></SUB> (t). The RSS between predicted and observed &Dgr;P<SUB><IT>f</IT></SUB> (t) was calculated. Values of model parameters (g, h, d, and X0) and dynamic passive pressure parameters (Ap and phip) were then adjusted according to the rules of a Levenberg-Marquardt heuristic search algorithm, and the processes were repeated iteratively until RSS was minimized. Median model parameter values obtained with this procedure in the 14 hearts are reported in Table 1.

                              
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Table 1.   Median model parameter values

Unlike the sinusoidal approximation of Eq. 18, which could be fit only to individual responses to a single perturbation, model Eqs. 9-13 are more general and could be fit to groups of responses to perturbations of multiple frequencies and amplitudes. By fitting simultaneously to responses to the 20 perturbations imposed in any one heart, we required this single model with a single set of parameters to account for a wide range of behaviors resulting from many different perturbations as in Fig. 2. Successful reproduction of this broad range of dynamic responses was taken as compelling evidence for validity of the basic model.

By all measures, the basic 2-state, 4-parameter model fit the response data very well. An example of this good fit in one heart is shown for a single heartbeat ( f = 50 Hz; Delta Vc = 1% VBL) in Fig. 5. In evaluating Fig. 5, it must be kept in mind that the fit that generated the predicted response was to responses obtained from the complete set of four frequencies and five amplitudes of inputs delivered to each of 20 beats and not just to the single beat shown in Fig. 5. Because rapid cycling at 50 Hz generated a dense pattern on display from which model-predicted and measured waveforms could not be discriminated, individual cycles in the response were identified that 1) spanned the point on the ascending limb of Pr(t) at which Pr(t) = 1/2 its peak value, 2) spanned the peak value of Pr(t), and 3) spanned the point on the descending limb at which Pr(t) = 1/2 its peak value. These three cycles were then expanded in row B of Fig. 5 such that predicted and observed waveforms could be compared. The comparatively small values of the differences between predicted and observed waveforms (residuals) are given in row C of Fig. 5. In this particular example, but not true in all cases, the residuals appeared to be random at all times during the heart period and exhibited no transient systematic character. Systematic patterns in the residuals will exhibit as a periodicity at the frequency of perturbation.


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Fig. 5.   A: response to a single perturbation f = 50 Hz; Delta Vc = 1% VBL. Model was fit to complete set of 4 frequencies and 5 amplitudes of inputs delivered to 20 beats, not just to single beat shown. B: model-predicted vs. measured waveforms. These overlain waveforms cannot be discriminated in left panel. Waveforms of single cycles (identified by period between pairs of vertical lines in left panel) are displayed in 3 panels to right. These cycles spanned: 1) the point on ascending limb of Pr(t) at which Pr(t) = 1/2 its peak value, 2) the peak value of Pr(t), and 3) the point on descending limb at which Pr(t) = 1/2 its peak value. C: residuals between model-predicted and observed waveforms. Residuals are small valued and do not have periodicity of perturbation. Thus, in this example, they are apparently random.

To demonstrate the goodness of the fit over the full set of 20 perturbed beats collected in the single heart featured in Fig. 5, predicted and measured values were plotted against one another to generate Fig. 6. In keeping with an R2 value of 0.98 in this heart, all the points cluster tightly around a line that is not clearly distinguishable from the line of identity. It can be seen that deviations of predicted from observed &Dgr;P<SUB><IT>fa</IT></SUB>(t) were never large, and an excellent fit was achieved at all frequencies and amplitudes of perturbation.


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Fig. 6.   Model predicted vs. measured &Dgr;P<SUB><IT>fa</IT></SUB>(t) for all 20 perturbed beats in one heart; 40,000 points shown (20 beats, each of 1-s duration, sampled at 2 kHz). Points in densest part of cluster around origin represent data generated at smallest Delta Vc, at lowest f, at lowest values of Pr(t), and during zero crossings at all perturbations. Points in less dense vertices of cluster represent data generated at highest Delta Vc, at highest f, and at peak of Pr(t). All points cluster tightly around line of identity. Deviations of predicted from observed &Dgr;P<SUB><IT>fa</IT></SUB>(t) were never large, and an excellent fit was achieved at all frequencies and amplitudes of perturbation.

An additional demonstration of model goodness of fit comes from comparing the actual responses displayed in Fig. 2 with the corresponding model-predicted responses displayed in the same format in Fig. 7. Visual comparison of these two figures reveals no important differences. Yet another demonstration of correspondence between model prediction and measured responses is seen in Fig. 8, where it is shown that there was good agreement between A1/Delta V for all 20 responses from the sinusoidal analysis and the 20 model-derived equivalents. This agreement was with respect to both absolute magnitudes and to systematic variations with f and Delta V, strong dependence on f, and little or no dependence on Delta V.


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Fig. 7.