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https://github.com/thestk/stk
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130 lines
3.5 KiB
C++
130 lines
3.5 KiB
C++
#ifndef STK_FLUTE_H
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#define STK_FLUTE_H
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#include "Instrmnt.h"
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#include "JetTable.h"
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#include "DelayL.h"
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#include "OnePole.h"
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#include "PoleZero.h"
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#include "Noise.h"
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#include "ADSR.h"
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#include "SineWave.h"
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namespace stk {
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/***************************************************/
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/*! \class Flute
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\brief STK flute physical model class.
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This class implements a simple flute
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physical model, as discussed by Karjalainen,
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Smith, Waryznyk, etc. The jet model uses
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a polynomial, a la Cook.
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This is a digital waveguide model, making its
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use possibly subject to patents held by Stanford
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University, Yamaha, and others.
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Control Change Numbers:
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- Jet Delay = 2
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- Noise Gain = 4
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- Vibrato Frequency = 11
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- Vibrato Gain = 1
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- Breath Pressure = 128
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by Perry R. Cook and Gary P. Scavone, 1995 - 2010.
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*/
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/***************************************************/
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class Flute : public Instrmnt
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{
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public:
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//! Class constructor, taking the lowest desired playing frequency.
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/*!
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An StkError will be thrown if the rawwave path is incorrectly set.
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*/
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Flute( StkFloat lowestFrequency );
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//! Class destructor.
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~Flute( void );
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//! Reset and clear all internal state.
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void clear( void );
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//! Set instrument parameters for a particular frequency.
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void setFrequency( StkFloat frequency );
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//! Set the reflection coefficient for the jet delay (-1.0 - 1.0).
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void setJetReflection( StkFloat coefficient );
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//! Set the reflection coefficient for the air column delay (-1.0 - 1.0).
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void setEndReflection( StkFloat coefficient );
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//! Set the length of the jet delay in terms of a ratio of jet delay to air column delay lengths.
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void setJetDelay( StkFloat aRatio );
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//! Apply breath velocity to instrument with given amplitude and rate of increase.
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void startBlowing( StkFloat amplitude, StkFloat rate );
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//! Decrease breath velocity with given rate of decrease.
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void stopBlowing( StkFloat rate );
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//! Start a note with the given frequency and amplitude.
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void noteOn( StkFloat frequency, StkFloat amplitude );
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//! Stop a note with the given amplitude (speed of decay).
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void noteOff( StkFloat amplitude );
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//! Perform the control change specified by \e number and \e value (0.0 - 128.0).
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void controlChange( int number, StkFloat value );
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//! Compute and return one output sample.
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StkFloat tick( unsigned int channel = 0 );
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protected:
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DelayL jetDelay_;
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DelayL boreDelay_;
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JetTable jetTable_;
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OnePole filter_;
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PoleZero dcBlock_;
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Noise noise_;
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ADSR adsr_;
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SineWave vibrato_;
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unsigned long length_;
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StkFloat lastFrequency_;
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StkFloat maxPressure_;
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StkFloat jetReflection_;
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StkFloat endReflection_;
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StkFloat noiseGain_;
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StkFloat vibratoGain_;
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StkFloat outputGain_;
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StkFloat jetRatio_;
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};
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inline StkFloat Flute :: tick( unsigned int )
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{
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StkFloat pressureDiff;
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StkFloat breathPressure;
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// Calculate the breath pressure (envelope + noise + vibrato)
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breathPressure = maxPressure_ * adsr_.tick();
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breathPressure += breathPressure * ( noiseGain_ * noise_.tick() + vibratoGain_ * vibrato_.tick() );
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StkFloat temp = filter_.tick( boreDelay_.lastOut() );
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temp = dcBlock_.tick( temp ); // Block DC on reflection.
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pressureDiff = breathPressure - (jetReflection_ * temp);
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pressureDiff = jetDelay_.tick( pressureDiff );
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pressureDiff = jetTable_.tick( pressureDiff ) + (endReflection_ * temp);
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lastFrame_[0] = (StkFloat) 0.3 * boreDelay_.tick( pressureDiff );
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lastFrame_[0] *= outputGain_;
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return lastFrame_[0];
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}
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} // stk namespace
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#endif
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