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Christoph Urlacher
2026-06-12 20:06:22 +02:00
parent 30daa8a00c
commit 08c2e9c13d
1122 changed files with 520422 additions and 0 deletions
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targets/wasm-tacle/parallel/rosace/thread3/assemblage.c Normal file
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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: assemblage.c
Author: Unknown
Function:
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/
c_posix_implementation/
Original name: assemblage.c
Changes: No major functional changes.
License: See the terms above.
*/
#include "assemblage.h"
#include "assemblage_includes.h"
// Definition of true and false here instead of using stdbool.h
#define true 1
#define false 0
double aircraft_dynamics495_Va_Va_filter_100449_Va[ 2 ];
double Vz_control_50483_delta_e_c_elevator489_delta_e_c;
double Va_filter_100449_Va_f_Va_control_50474_Va_f[ 2 ];
double Vz_filter_100452_Vz_f_Va_control_50474_Vz_f[ 2 ];
double q_filter_100455_q_f_Va_control_50474_q_f[ 2 ];
double Va_c_Va_control_50474_Va_c;
double h_filter_100446_h_f_altitude_hold_50464_h_f[ 2 ];
double h_c_altitude_hold_50464_h_c;
double Va_control_50474_delta_th_c_delta_th_c;
double aircraft_dynamics495_az_az_filter_100458_az[ 2 ];
double aircraft_dynamics495_Vz_Vz_filter_100452_Vz[ 2 ];
double aircraft_dynamics495_q_q_filter_100455_q[ 2 ];
double elevator489_delta_e_aircraft_dynamics495_delta_e[ 3 ] = {0.0120096156525, 0.0120096156525, 0.0120096156525};
double engine486_T_aircraft_dynamics495_T[ 3 ] = {41813.9211946, 41813.9211946, 41813.9211946};
double aircraft_dynamics495_h_h_filter_100446_h[ 2 ];
double Va_control_50474_delta_th_c_engine486_delta_th_c;
double Vz_filter_100452_Vz_f_Vz_control_50483_Vz_f[ 2 ];
double altitude_hold_50464_Vz_c_Vz_control_50483_Vz_c;
double q_filter_100455_q_f_Vz_control_50483_q_f[ 2 ];
double az_filter_100458_az_f_Vz_control_50483_az_f[ 2 ];
double Vz_control_50483_delta_e_c_delta_e_c;
int Va_filter_100449_fun( void *args )
{
double Va_f;
static int Va_rcell = 0;
const struct write_proto_t Va_f_Va_control_50474_Va_f_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int Va_f_Va_control_50474_Va_f_wcell = 0;
static int instance = 0;
Va_f = Va_filter_100( aircraft_dynamics495_Va_Va_filter_100449_Va[ Va_rcell ] );
Va_rcell = ( Va_rcell + 1 ) % 2;
if ( must_write( Va_f_Va_control_50474_Va_f_write, instance ) ) {
Va_filter_100449_Va_f_Va_control_50474_Va_f[ Va_f_Va_control_50474_Va_f_wcell ] =
Va_f;
Va_f_Va_control_50474_Va_f_wcell = ( Va_f_Va_control_50474_Va_f_wcell + 1 ) % 2;
}
instance++;
return 0;
}
int elevator489_fun( void *args )
{
double delta_e;
static int delta_e_aircraft_dynamics495_delta_e_wcell = 1;
static int instance = 0;
delta_e = elevator( Vz_control_50483_delta_e_c_elevator489_delta_e_c );
elevator489_delta_e_aircraft_dynamics495_delta_e[ delta_e_aircraft_dynamics495_delta_e_wcell ]
= delta_e;
delta_e_aircraft_dynamics495_delta_e_wcell =
( delta_e_aircraft_dynamics495_delta_e_wcell + 1 ) % 3;
instance++;
return 0;
}
int Va_control_50474_fun( void *args )
{
double delta_th_c;
static int Va_f_rcell = 0;
static int Vz_f_rcell = 0;
static int q_f_rcell = 0;
static int instance = 0;
delta_th_c = Va_control_50(
Va_filter_100449_Va_f_Va_control_50474_Va_f[ Va_f_rcell ],
Vz_filter_100452_Vz_f_Va_control_50474_Vz_f[ Vz_f_rcell ],
q_filter_100455_q_f_Va_control_50474_q_f[ q_f_rcell ],
Va_c_Va_control_50474_Va_c );
Va_f_rcell = ( Va_f_rcell + 1 ) % 2;
Vz_f_rcell = ( Vz_f_rcell + 1 ) % 2;
q_f_rcell = ( q_f_rcell + 1 ) % 2;
Va_control_50474_delta_th_c_engine486_delta_th_c = delta_th_c;
Va_control_50474_delta_th_c_delta_th_c = delta_th_c;
instance++;
return 0;
}
int Va_c0_fun( void *args )
{
double Va_c;
static int instance = 0;
Va_c = input_Va_c();
Va_c_Va_control_50474_Va_c = Va_c;
instance++;
return 0;
}
int altitude_hold_50464_fun( void *args )
{
double Vz_c;
static int h_f_rcell = 0;
static int instance = 0;
Vz_c = altitude_hold_50( h_filter_100446_h_f_altitude_hold_50464_h_f[ h_f_rcell ],
h_c_altitude_hold_50464_h_c );
h_f_rcell = ( h_f_rcell + 1 ) % 2;
altitude_hold_50464_Vz_c_Vz_control_50483_Vz_c = Vz_c;
instance++;
return 0;
}
int delta_th_c0_fun( void *args )
{
static int instance = 0;
output_delta_th_c( Va_control_50474_delta_th_c_delta_th_c );
instance++;
return 0;
}
int az_filter_100458_fun( void *args )
{
double az_f;
static int az_rcell = 0;
const struct write_proto_t az_f_Vz_control_50483_az_f_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int az_f_Vz_control_50483_az_f_wcell = 0;
static int instance = 0;
az_f = az_filter_100( aircraft_dynamics495_az_az_filter_100458_az[ az_rcell ] );
az_rcell = ( az_rcell + 1 ) % 2;
if ( must_write( az_f_Vz_control_50483_az_f_write, instance ) ) {
az_filter_100458_az_f_Vz_control_50483_az_f[ az_f_Vz_control_50483_az_f_wcell ] =
az_f;
az_f_Vz_control_50483_az_f_wcell = ( az_f_Vz_control_50483_az_f_wcell + 1 ) % 2;
}
instance++;
return 0;
}
int Vz_filter_100452_fun( void *args )
{
double Vz_f;
static int Vz_rcell = 0;
const struct write_proto_t Vz_f_Va_control_50474_Vz_f_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int Vz_f_Va_control_50474_Vz_f_wcell = 0;
const struct write_proto_t Vz_f_Vz_control_50483_Vz_f_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int Vz_f_Vz_control_50483_Vz_f_wcell = 0;
static int instance = 0;
Vz_f = Vz_filter_100( aircraft_dynamics495_Vz_Vz_filter_100452_Vz[ Vz_rcell ] );
Vz_rcell = ( Vz_rcell + 1 ) % 2;
if ( must_write( Vz_f_Va_control_50474_Vz_f_write, instance ) ) {
Vz_filter_100452_Vz_f_Va_control_50474_Vz_f[ Vz_f_Va_control_50474_Vz_f_wcell ] =
Vz_f;
Vz_f_Va_control_50474_Vz_f_wcell = ( Vz_f_Va_control_50474_Vz_f_wcell + 1 ) % 2;
}
if ( must_write( Vz_f_Vz_control_50483_Vz_f_write, instance ) ) {
Vz_filter_100452_Vz_f_Vz_control_50483_Vz_f[ Vz_f_Vz_control_50483_Vz_f_wcell ] =
Vz_f;
Vz_f_Vz_control_50483_Vz_f_wcell = ( Vz_f_Vz_control_50483_Vz_f_wcell + 1 ) % 2;
}
instance++;
return 0;
}
int q_filter_100455_fun( void *args )
{
double q_f;
static int q_rcell = 0;
const struct write_proto_t q_f_Va_control_50474_q_f_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int q_f_Va_control_50474_q_f_wcell = 0;
const struct write_proto_t q_f_Vz_control_50483_q_f_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int q_f_Vz_control_50483_q_f_wcell = 0;
static int instance = 0;
q_f = q_filter_100( aircraft_dynamics495_q_q_filter_100455_q[ q_rcell ] );
q_rcell = ( q_rcell + 1 ) % 2;
if ( must_write( q_f_Va_control_50474_q_f_write, instance ) ) {
q_filter_100455_q_f_Va_control_50474_q_f[ q_f_Va_control_50474_q_f_wcell ] = q_f;
q_f_Va_control_50474_q_f_wcell = ( q_f_Va_control_50474_q_f_wcell + 1 ) % 2;
}
if ( must_write( q_f_Vz_control_50483_q_f_write, instance ) ) {
q_filter_100455_q_f_Vz_control_50483_q_f[ q_f_Vz_control_50483_q_f_wcell ] = q_f;
q_f_Vz_control_50483_q_f_wcell = ( q_f_Vz_control_50483_q_f_wcell + 1 ) % 2;
}
instance++;
return 0;
}
int aircraft_dynamics495_fun( void *args )
{
struct aircraft_dynamics_outs_t aircraft_dynamics495_fun_outs;
static int delta_e_rcell = 0;
static int T_rcell = 0;
const struct write_proto_t Va_Va_filter_100449_Va_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int Va_Va_filter_100449_Va_wcell = 0;
const struct write_proto_t Vz_Vz_filter_100452_Vz_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int Vz_Vz_filter_100452_Vz_wcell = 0;
const struct write_proto_t q_q_filter_100455_q_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int q_q_filter_100455_q_wcell = 0;
const struct write_proto_t az_az_filter_100458_az_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int az_az_filter_100458_az_wcell = 0;
const struct write_proto_t h_h_filter_100446_h_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int h_h_filter_100446_h_wcell = 0;
static int instance = 0;
aircraft_dynamics(
elevator489_delta_e_aircraft_dynamics495_delta_e[ delta_e_rcell ],
engine486_T_aircraft_dynamics495_T[ T_rcell ], &aircraft_dynamics495_fun_outs );
delta_e_rcell = ( delta_e_rcell + 1 ) % 3;
T_rcell = ( T_rcell + 1 ) % 3;
if ( must_write( Va_Va_filter_100449_Va_write, instance ) ) {
aircraft_dynamics495_Va_Va_filter_100449_Va[ Va_Va_filter_100449_Va_wcell ] =
aircraft_dynamics495_fun_outs.Va;
Va_Va_filter_100449_Va_wcell = ( Va_Va_filter_100449_Va_wcell + 1 ) % 2;
}
if ( must_write( Vz_Vz_filter_100452_Vz_write, instance ) ) {
aircraft_dynamics495_Vz_Vz_filter_100452_Vz[ Vz_Vz_filter_100452_Vz_wcell ] =
aircraft_dynamics495_fun_outs.Vz;
Vz_Vz_filter_100452_Vz_wcell = ( Vz_Vz_filter_100452_Vz_wcell + 1 ) % 2;
}
if ( must_write( q_q_filter_100455_q_write, instance ) ) {
aircraft_dynamics495_q_q_filter_100455_q[ q_q_filter_100455_q_wcell ] =
aircraft_dynamics495_fun_outs.q;
q_q_filter_100455_q_wcell = ( q_q_filter_100455_q_wcell + 1 ) % 2;
}
if ( must_write( az_az_filter_100458_az_write, instance ) ) {
aircraft_dynamics495_az_az_filter_100458_az[ az_az_filter_100458_az_wcell ] =
aircraft_dynamics495_fun_outs.az;
az_az_filter_100458_az_wcell = ( az_az_filter_100458_az_wcell + 1 ) % 2;
}
if ( must_write( h_h_filter_100446_h_write, instance ) ) {
aircraft_dynamics495_h_h_filter_100446_h[ h_h_filter_100446_h_wcell ] =
aircraft_dynamics495_fun_outs.h;
h_h_filter_100446_h_wcell = ( h_h_filter_100446_h_wcell + 1 ) % 2;
}
instance++;
return 0;
}
int h_filter_100446_fun( void *args )
{
double h_f;
static int h_rcell = 0;
const struct write_proto_t h_f_altitude_hold_50464_h_f_write =
{ NULL, 0, ( int [] ){ true, false }, 2 };
static int h_f_altitude_hold_50464_h_f_wcell = 0;
static int instance = 0;
h_f = h_filter_100( aircraft_dynamics495_h_h_filter_100446_h[ h_rcell ] );
h_rcell = ( h_rcell + 1 ) % 2;
if ( must_write( h_f_altitude_hold_50464_h_f_write, instance ) ) {
h_filter_100446_h_f_altitude_hold_50464_h_f[ h_f_altitude_hold_50464_h_f_wcell ] =
h_f;
h_f_altitude_hold_50464_h_f_wcell = ( h_f_altitude_hold_50464_h_f_wcell + 1 ) %
2;
}
instance++;
return 0;
}
int engine486_fun( void *args )
{
double T;
static int T_aircraft_dynamics495_T_wcell = 1;
static int instance = 0;
T = engine( Va_control_50474_delta_th_c_engine486_delta_th_c );
engine486_T_aircraft_dynamics495_T[ T_aircraft_dynamics495_T_wcell ] = T;
T_aircraft_dynamics495_T_wcell = ( T_aircraft_dynamics495_T_wcell + 1 ) % 3;
instance++;
return 0;
}
int Vz_control_50483_fun( void *args )
{
double delta_e_c;
static int Vz_f_rcell = 0;
static int q_f_rcell = 0;
static int az_f_rcell = 0;
static int instance = 0;
delta_e_c = Vz_control_50(
Vz_filter_100452_Vz_f_Vz_control_50483_Vz_f[ Vz_f_rcell ],
altitude_hold_50464_Vz_c_Vz_control_50483_Vz_c,
q_filter_100455_q_f_Vz_control_50483_q_f[ q_f_rcell ],
az_filter_100458_az_f_Vz_control_50483_az_f[ az_f_rcell ] );
Vz_f_rcell = ( Vz_f_rcell + 1 ) % 2;
q_f_rcell = ( q_f_rcell + 1 ) % 2;
az_f_rcell = ( az_f_rcell + 1 ) % 2;
Vz_control_50483_delta_e_c_delta_e_c = delta_e_c;
Vz_control_50483_delta_e_c_elevator489_delta_e_c = delta_e_c;
instance++;
return 0;
}
int delta_e_c0_fun( void *args )
{
static int instance = 0;
output_delta_e_c( Vz_control_50483_delta_e_c_delta_e_c );
instance++;
return 0;
}
int h_c0_fun( void *args )
{
double h_c;
static int instance = 0;
h_c = input_h_c();
h_c_altitude_hold_50464_h_c = h_c;
instance++;
return 0;
}
#define PLUD_TASK_NUMBER 15
static struct nonencoded_task_params static_task_set[ PLUD_TASK_NUMBER ] = {
{ "h_c0", 1000, 0, 1, 1000, h_c0_fun },
{ "delta_e_c0", 200, 0, 1, 200, delta_e_c0_fun },
{ "Vz_control_50483", 200, 0, 1, 200, Vz_control_50483_fun },
{ "engine486", 50, 0, 1, 50, engine486_fun },
{ "h_filter_100446", 100, 0, 1, 100, h_filter_100446_fun },
{ "aircraft_dynamics495", 50, 0, 1, 50, aircraft_dynamics495_fun },
{ "q_filter_100455", 100, 0, 1, 100, q_filter_100455_fun },
{ "Vz_filter_100452", 100, 0, 1, 100, Vz_filter_100452_fun },
{ "az_filter_100458", 100, 0, 1, 100, az_filter_100458_fun },
{ "delta_th_c0", 200, 0, 1, 200, delta_th_c0_fun },
{ "altitude_hold_50464", 200, 0, 1, 200, altitude_hold_50464_fun },
{ "Va_c0", 1000, 0, 1, 1000, Va_c0_fun },
{ "Va_control_50474", 200, 0, 1, 200, Va_control_50474_fun },
{ "elevator489", 50, 0, 1, 50, elevator489_fun },
{ "Va_filter_100449", 100, 0, 1, 100, Va_filter_100449_fun }
};
void get_task_set ( int *task_number, struct nonencoded_task_params **task_set )
{
*task_number = PLUD_TASK_NUMBER;
*task_set = static_task_set;
}
static struct job_prec engine486_aircraft_dynamics495_pcpat[ 1 ] = { {0, 1} };
static struct job_prec Va_filter_100449_Va_control_50474_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec q_filter_100455_Va_control_50474_pcpat[ 1 ] = { {0, 0} };
static struct job_prec q_filter_100455_Vz_control_50483_pcpat[ 1 ] = { {0, 0} };
static struct job_prec aircraft_dynamics495_q_filter_100455_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec Va_c0_Va_control_50474_pcpat[ 1 ] = { {0, 0} };
static struct job_prec Vz_control_50483_delta_e_c0_pcpat[ 1 ] = { {0, 0} };
static struct job_prec Vz_control_50483_elevator489_pcpat[ 1 ] = { {0, 0} };
static struct job_prec Vz_filter_100452_Va_control_50474_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec Vz_filter_100452_Vz_control_50483_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec h_filter_100446_altitude_hold_50464_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec aircraft_dynamics495_az_filter_100458_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec elevator489_aircraft_dynamics495_pcpat[ 1 ] = { {0, 1} };
static struct job_prec aircraft_dynamics495_Vz_filter_100452_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec az_filter_100458_Vz_control_50483_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec h_c0_altitude_hold_50464_pcpat[ 1 ] = { {0, 0} };
static struct job_prec altitude_hold_50464_Vz_control_50483_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec aircraft_dynamics495_Va_filter_100449_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec aircraft_dynamics495_h_filter_100446_pcpat[ 1 ] = {
{0, 0}
};
static struct job_prec Va_control_50474_engine486_pcpat[ 1 ] = { {0, 0} };
static struct job_prec Va_control_50474_delta_th_c0_pcpat[ 1 ] = { {0, 0} };
#define PLUD_PREC_NUMBER 21
static struct multirate_precedence static_prec_set[ PLUD_PREC_NUMBER ] = {
{
"engine486", "aircraft_dynamics495", 0, 1, NULL,
engine486_aircraft_dynamics495_pcpat
},
{
"Va_filter_100449", "Va_control_50474", 0, 1, NULL,
Va_filter_100449_Va_control_50474_pcpat
},
{
"q_filter_100455", "Va_control_50474", 0, 1, NULL,
q_filter_100455_Va_control_50474_pcpat
},
{
"q_filter_100455", "Vz_control_50483", 0, 1, NULL,
q_filter_100455_Vz_control_50483_pcpat
},
{
"aircraft_dynamics495", "q_filter_100455", 0, 1, NULL,
aircraft_dynamics495_q_filter_100455_pcpat
},
{ "Va_c0", "Va_control_50474", 0, 1, NULL, Va_c0_Va_control_50474_pcpat },
{
"Vz_control_50483", "delta_e_c0", 0, 1, NULL,
Vz_control_50483_delta_e_c0_pcpat
},
{
"Vz_control_50483", "elevator489", 0, 1, NULL,
Vz_control_50483_elevator489_pcpat
},
{
"Vz_filter_100452", "Va_control_50474", 0, 1, NULL,
Vz_filter_100452_Va_control_50474_pcpat
},
{
"Vz_filter_100452", "Vz_control_50483", 0, 1, NULL,
Vz_filter_100452_Vz_control_50483_pcpat
},
{
"h_filter_100446", "altitude_hold_50464", 0, 1, NULL,
h_filter_100446_altitude_hold_50464_pcpat
},
{
"aircraft_dynamics495", "az_filter_100458", 0, 1, NULL,
aircraft_dynamics495_az_filter_100458_pcpat
},
{
"elevator489", "aircraft_dynamics495", 0, 1, NULL,
elevator489_aircraft_dynamics495_pcpat
},
{
"aircraft_dynamics495", "Vz_filter_100452", 0, 1, NULL,
aircraft_dynamics495_Vz_filter_100452_pcpat
},
{
"az_filter_100458", "Vz_control_50483", 0, 1, NULL,
az_filter_100458_Vz_control_50483_pcpat
},
{
"h_c0", "altitude_hold_50464", 0, 1, NULL, h_c0_altitude_hold_50464_pcpat
},
{
"altitude_hold_50464", "Vz_control_50483", 0, 1, NULL,
altitude_hold_50464_Vz_control_50483_pcpat
},
{
"aircraft_dynamics495", "Va_filter_100449", 0, 1, NULL,
aircraft_dynamics495_Va_filter_100449_pcpat
},
{
"aircraft_dynamics495", "h_filter_100446", 0, 1, NULL,
aircraft_dynamics495_h_filter_100446_pcpat
},
{
"Va_control_50474", "engine486", 0, 1, NULL,
Va_control_50474_engine486_pcpat
},
{
"Va_control_50474", "delta_th_c0", 0, 1, NULL,
Va_control_50474_delta_th_c0_pcpat
}
};
void get_precedence_set ( int *prec_number,
struct multirate_precedence **prec_set )
{
*prec_number = PLUD_PREC_NUMBER;
*prec_set = static_prec_set;
}

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: assemblage.h
Author: Unknown
Function:
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/
c_posix_implementation/
Original name: assemblage.h
Changes: No major functional changes.
License: See the terms above.
*/
#ifndef _assemblage_H
#define _assemblage_H
#include "nonencoded_task_params.h"
#include "multirate_precedence.h"
#include "com_patterns.h"
#include "types.h"
void get_task_set( int *task_number, struct nonencoded_task_params **task_set );
void get_precedence_set( int *prec_number,
struct multirate_precedence **presc );
#define H_C0 0
#define DELTA_E_C0 1
#define VZ_CONTROL 2
#define ENGINE 3
#define H_FILTER 4
#define AIRCRAFT_DYN 5
#define Q_FILTER 6
#define VZ_FILTER 7
#define AZ_FILTER 8
#define DELTA_TH_C0 9
#define ALTI_HOLD 10
#define VA_C0 11
#define VA_CONTROL 12
#define ELEVATOR 13
#define VA_FILTER 14
#endif

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: assemblage_includes.h
Author: Unknown
Function:
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/
c_posix_implementation/
Original name: assemblage_includes.h
Changes: No major functional changes.
License: See the terms above.
*/
#ifndef ASSEMBLAGE_INCLUDES_H
#define ASSEMBLAGE_INCLUDES_H
#include "types.h"
#include "io.h"
/* ***************************************************************************
Shared constants
* ************************************************************************* */
#define delta_th_eq (1.5868660794926)
#define delta_e_eq (0.012009615652468)
extern const REAL_TYPE h_eq;
extern const REAL_TYPE Va_eq;
#ifndef NBMAX_SAMPLE
#define NBMAX_SAMPLE (6000000/4)
#endif
extern REAL_TYPE sample[ SPL_SIZE ][ NBMAX_SAMPLE ];
void print_inmemory_sample( void );
/* ***************************************************************************
The prelude imported node prototypes
* ************************************************************************* */
/**
Va filter (100/50/33/25 Hz --> 10/20/30/40 ms period)
@param[in] Va, airspeed (m/s)
@return Va_f, filtered airspeed (m/s)
2nd order Butterworth filter with fc = 0.5 Hz (Matlab function butter)
Discretized with Zero-order Hold method with Ts = 0.01/0.02/0.03/0.04 (Matlab function c2d)
*/
REAL_TYPE
Va_filter_100( REAL_TYPE Va );
REAL_TYPE
Va_filter_50( REAL_TYPE Va );
REAL_TYPE
Va_filter_33( REAL_TYPE Va );
REAL_TYPE
Va_filter_25( REAL_TYPE Va );
/**
Vz filter (100/50/33/25 Hz --> 10/20/30/40 ms period)
@param[in] Vz, vertical speed (m/s)
@return Vz_f, filtered vertical airspeed (m/s)
2nd order Butterworth filter with fc = 0.5 Hz (Matlab function butter)
Discretized with Zero-order Hold method with Ts = 0.01/0.02/0.03/0.04 (Matlab function c2d)
*/
REAL_TYPE
Vz_filter_100( REAL_TYPE Vz );
REAL_TYPE
Vz_filter_50 ( REAL_TYPE Vz );
REAL_TYPE
Vz_filter_33 ( REAL_TYPE Vz );
REAL_TYPE
Vz_filter_25 ( REAL_TYPE Vz );
/**
q filter (100/50/33/25 Hz --> 10/20/30/40 ms period)
@param[in] q, pitch rate (rad/s)
@return q_f, filtered pitch rate (rad/s)
2nd order Butterworth filter with fc = 3.0 Hz (Matlab function butter)
Discretized with Zero-order Hold method with Ts = 0.01/0.02/0.03/0.04 (Matlab function c2d)
*/
REAL_TYPE
q_filter_100( REAL_TYPE q );
REAL_TYPE
q_filter_50 ( REAL_TYPE q );
REAL_TYPE
q_filter_33 ( REAL_TYPE q );
REAL_TYPE
q_filter_25 ( REAL_TYPE q );
/**
az filter (100/50/33/25 Hz --> 10/20/30/40 ms period)
@param[in] az, normal acceleration (m/s^2)
@return az_f, filtered normal acceleration (m/s^2)
2nd order Butterworth filter with fc = 10.0 Hz (Matlab function butter)
Discretized with Zero-order Hold method with Ts = 0.01/0.02/0.03/0.04 (Matlab function c2d)
*/
REAL_TYPE
az_filter_100( REAL_TYPE az );
REAL_TYPE
az_filter_50 ( REAL_TYPE az );
REAL_TYPE
az_filter_33 ( REAL_TYPE az );
REAL_TYPE
az_filter_25 ( REAL_TYPE az );
/**
h filter (100/50/33/25 Hz --> 10/20/30/40 ms period)
@param[in] h, altitude (m)
@return h_f, filtered altitude (m)
2nd order Butterworth filter with fc = 3.0 Hz (Matlab function butter)
Discretized with Zero-order Hold method with Ts = 0.01/0.02/0.03/0.04 (Matlab function c2d)
*/
REAL_TYPE
h_filter_100( REAL_TYPE h );
REAL_TYPE
h_filter_50 ( REAL_TYPE h );
REAL_TYPE
h_filter_33 ( REAL_TYPE h );
REAL_TYPE
h_filter_25 ( REAL_TYPE h );
/**
Altitude hold controller (rate 50/33/25/10 Hz sampling period 0.02/0.03/0.04/0.1)
@param[in] h_f, filtered altitude (m)
@param[in] h_c, commanded altitude (m)
@return Vz_c, commanded vertical speed (m/s)
Generates the vertical speed command Vz_c to track altitude change h_c
*/
REAL_TYPE
altitude_hold_50 ( REAL_TYPE h_f, REAL_TYPE h_c );
REAL_TYPE
altitude_hold_33 ( REAL_TYPE h_f, REAL_TYPE h_c );
REAL_TYPE
altitude_hold_25 ( REAL_TYPE h_f, REAL_TYPE h_c );
REAL_TYPE
altitude_hold_10 ( REAL_TYPE h_f, REAL_TYPE h_c );
/**
Vz Speed controller (rate 50/33/25/10 Hz sampling period 0.02/0.03/0.04/0.1)
@param[in] Vz_f, filtered vertical speed (m/s)
@param[in] Vz_c, commanded vertical speed (m/s)
@param[in] q_f, filtered pitch rate (rad/s)
@param[in] az_f, filtered normal acceleration (m/s^2)
@return delta_e_c, commanded elevator deflection (rad)
Generates the elevator deflection command to track vertical speed command Vz_c
*/
REAL_TYPE
Vz_control_50 ( REAL_TYPE Vz_f, REAL_TYPE Vz_c,
REAL_TYPE q_f, REAL_TYPE az_f );
REAL_TYPE
Vz_control_33 ( REAL_TYPE Vz_f, REAL_TYPE Vz_c,
REAL_TYPE q_f, REAL_TYPE az_f );
REAL_TYPE
Vz_control_25 ( REAL_TYPE Vz_f, REAL_TYPE Vz_c,
REAL_TYPE q_f, REAL_TYPE az_f );
REAL_TYPE
Vz_control_10 ( REAL_TYPE Vz_f, REAL_TYPE Vz_c,
REAL_TYPE q_f, REAL_TYPE az_f );
/**
Va Speed controller (rate 50/33/25/10 Hz sampling period 0.02/0.03/0.04/0.1)
@param[in] Va_f, filtered airspeed (m/s)
@param[in] Vz_f, filtered vertical speed (m/s)
@param[in] q_f, filtered pitch rate (rad/s)
@return delta_th_c, commanded throttle (-)
Generates the throttle command to track airspeed change Va_c
*/
REAL_TYPE
Va_control_50 ( REAL_TYPE Va_f, REAL_TYPE Vz_f,
REAL_TYPE q_f, REAL_TYPE Va_c );
REAL_TYPE
Va_control_33 ( REAL_TYPE Va_f, REAL_TYPE Vz_f,
REAL_TYPE q_f, REAL_TYPE Va_c );
REAL_TYPE
Va_control_25 ( REAL_TYPE Va_f, REAL_TYPE Vz_f,
REAL_TYPE q_f, REAL_TYPE Va_c );
REAL_TYPE
Va_control_10 ( REAL_TYPE Va_f, REAL_TYPE Vz_f,
REAL_TYPE q_f, REAL_TYPE Va_c );
/**
Engine (200 Hz --> 5ms period)
@param[in] delta_th_c, commanded throttle (-)
@return T, Thrust (N)
1st order system with time constant 0.5 s
ODE Solver: Euler method with fixed-step = 0.005 (200 Hz)
*/
REAL_TYPE
engine( REAL_TYPE delta_th_c );
/**
Elevator (200 Hz --> 5ms period)
@param[in] delta_e_c, commanded elevator deflection (rad)
@return delta_e, elevator deflection (rad)
2nd order system (natural frequency omega = 25.0 rad/s and damping xi = 0.85)
ODE Solver: Euler method with fixed-step = 0.005 s (200 Hz)
*/
REAL_TYPE
elevator( REAL_TYPE delta_e_c );
/**
Flight dynamics (200 Hz --> 5ms period)
@param[in] i, the simulation step
@param[in] delta_e, elevator deflection (rad)
@param[in] T, Thrust (N)
@param[out] outputs, the outputs Va, Vz, q, az, h
Aircraft flight dynamics
ODE Solver: Euler method with fixed-step = 0.005 s (200 Hz)
*/
void
aircraft_dynamics ( REAL_TYPE delta_e, REAL_TYPE T,
struct aircraft_dynamics_outs_t *outputs );
/* ***************************************************************************
The prelude sensor node prototypes
* ************************************************************************* */
/**
(200 Hz --> 5ms period)
*/
REAL_TYPE
input_h_c( void );
REAL_TYPE
input_Va_c( void );
/* ***************************************************************************
The prelude actuator node prototypes
* ************************************************************************* */
/**
(200 Hz --> 5ms period)
*/
void
output_delta_th_c( REAL_TYPE delta_th_c );
/**
(200 Hz --> 5ms period)
*/
void
output_delta_e_c( REAL_TYPE delta_e_c );
#endif

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: com_patterns.h
Author: Unknown
Function:
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/
c_posix_implementation/
Original name: com_patterns.h
Changes: No major functional changes.
License: See the terms above.
*/
#ifndef com_patterns_H_
#define com_patterns_H_
// Description of communication protocols using ultimately periodic
// words: prefix.(periodic pattern). Each communication uses a circular
// buffer shared between the writer and the reader.
// The task instance i writes to the communication buffer iff proto[n]
// is true (modulo the size of the periodic word). After each write, the
// index where the writer writes is incremented.
struct write_proto_t {
int *write_pref;
int wpref_size;
int *write_pat;
int wpat_size;
};
// The task instance n must increment the index at which the task reads
// in the communication buffer iff proto[n] is true (modulo the size of the
// periodic word).
struct read_proto_t {
int *change_pref;
int rpref_size;
int *change_pat;
int rpat_size;
};
/**
Returns 1 if instance n must write in the com buffer.
*/
static inline int must_write( struct write_proto_t wp, int n )
{
if ( n < wp.wpref_size )
return wp.write_pref[ n ];
else
return wp.write_pat[ ( n - wp.wpref_size ) % wp.wpat_size ];
}
/**
Returns 1 if instance n must change the cell from which it reads.
*/
static inline int must_change( struct read_proto_t rp, int n )
{
if ( n < rp.rpref_size )
return rp.change_pref[ n ];
else
return rp.change_pat[ ( n - rp.rpref_size ) % rp.rpat_size ];
}
#endif

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: common.c
Author: Dustin Green
Function: Common used functions from original threads.c
Source:
Original name:
Changes: No major changes of functions from original threads.c
License: See the terms above.
*/
#include "common.h"
#include "types.h"
#include "assemblage_includes.h"
#include "assemblage.h"
void rosace_init( void )
{
// Initial values
outs.sig_outputs.Va = 0;
outs.sig_outputs.Vz = 0;
outs.sig_outputs.q = 0;
outs.sig_outputs.az = 0;
outs.sig_outputs.h = 0;
outs.t_simu = 0;
step_simu = 0;
// Get the task set (required for CALL() macro)
int tmp;
get_task_set( &tmp, &tasks );
}
void copy_output_vars( output_t *v, uint64_t step )
{
v->sig_outputs.Va = aircraft_dynamics495_Va_Va_filter_100449_Va[ step % 2 ];
v->sig_outputs.Vz = aircraft_dynamics495_Vz_Vz_filter_100452_Vz[ step % 2 ];
v->sig_outputs.q = aircraft_dynamics495_q_q_filter_100455_q[ step % 2 ];
v->sig_outputs.az = aircraft_dynamics495_az_az_filter_100458_az[ step % 2 ];
v->sig_outputs.h = aircraft_dynamics495_h_h_filter_100446_h[ step % 2 ];
v->sig_delta_th_c = Va_control_50474_delta_th_c_delta_th_c;
v->sig_delta_e_c = Vz_control_50483_delta_e_c_delta_e_c;
}

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: common.h
Author: Dustin Green
Function: Common used functions and variables from original threads.c
Source:
Original name:
Changes: No major functional changes
License: See the terms above.
*/
#ifndef COMMON_H
#define COMMON_H
#include "types.h"
#include "assemblage_includes.h"
#include "assemblage.h"
// I/O
output_t outs;
uint64_t step_simu;
uint64_t max_step_simu;
// Output variables
extern double aircraft_dynamics495_Va_Va_filter_100449_Va[ 2 ];
extern double aircraft_dynamics495_az_az_filter_100458_az[ 2 ];
extern double aircraft_dynamics495_Vz_Vz_filter_100452_Vz[ 2 ];
extern double aircraft_dynamics495_q_q_filter_100455_q[ 2 ];
extern double aircraft_dynamics495_h_h_filter_100446_h[ 2 ];
extern double Va_control_50474_delta_th_c_delta_th_c;
extern double Vz_control_50483_delta_e_c_delta_e_c;
// Task set
struct nonencoded_task_params *tasks;
// Common functions
void rosace_init( void );
void copy_output_vars( output_t *v, uint64_t step );
// This should be set to 1 to run in "real-time" in the sense
// that the simulation time is close to the real world time
#define RUN_WITH_REAL_TIME 0
#define CALL( val ) tasks[ (val) ].ne_t_body( NULL )
#endif

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: io.c
Author: Unknown
Function: Output function
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/
c_posix_implementation/
Original name: io.c
Changes: delete the code within ROSACE_write_outputs because
stdio.h is not available
License: See the terms above.
*/
#include "types.h"
#include "io.h"
#define FMTREAL "%5.15f"
#define BASE_FREQUENCY 200.0
extern REAL_TYPE h_c;
void ROSACE_update_altitude_command( REAL_TYPE h_cons )
{
h_c = h_cons;
}
void ROSACE_write_outputs( output_t *v )
{
}

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: io.h
Author: Unknown
Function: Output function
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/
c_posix_implementation/
Original name: io.h
Changes: No major functional changes.
License: See the terms above.
*/
#ifndef __DEF_ROSACE_IO_H
#define __DEF_ROSACE_IO_H
#include "types.h"
typedef struct {
struct aircraft_dynamics_outs_t sig_outputs;
uint64_t t_simu;
REAL_TYPE sig_delta_th_c;
REAL_TYPE sig_delta_e_c;
} output_t;
void ROSACE_write_outputs( output_t *v );
void ROSACE_update_altitude_command( REAL_TYPE h_cons );
#endif

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/*
====================================================
Copyright (C) 1993 by Sun Microsystems, Inc. All rights reserved.
Developed at SunPro, a Sun Microsystems, Inc. business.
Permission to use, copy, modify, and distribute this
software is freely granted, provided that this notice
is preserved.
====================================================
*/
/*
from: @(#)fdlibm.h 5.1 93/09/24
*/
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: math_private.h
Author: Unknown
Function: IEEE754 software library routines.
Source: Sun Microsystems
Original name: fdlibm.h
Changes: No major functional changes.
License: See the terms above.
*/
#ifndef _MATH_PRIVATE_H_
#define _MATH_PRIVATE_H_
#include "wcclibm.h"
/* A union which permits us to convert between a float and a 32 bit int. */
typedef union {
float value;
u_int32_t word;
} ieee_float_shape_type;
/* Get a 32 bit int from a float. */
#define GET_FLOAT_WORD(i,d) \
{ \
ieee_float_shape_type gf_u; \
gf_u.value = ( d ); \
( i ) = gf_u.word; \
}
/* Set a float from a 32 bit int. */
#define SET_FLOAT_WORD( d, i ) \
{ \
ieee_float_shape_type sf_u; \
sf_u.word = ( i ); \
( d ) = sf_u.value; \
}
#endif /* _MATH_PRIVATE_H_ */

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: multirate_precedence.h
Author: Unknown
Function:
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/
c_posix_implementation/
Original name: multirate_precedence.h
Changes: No major functional changes.
License: See the terms above.
*/
#ifndef _multirate_precedence_H
#define _multirate_precedence_H
#include <stdlib.h>
// Description of a precedence between two tasks of different rates
struct job_prec {
int src_job;
int dst_job;
};
struct multirate_precedence {
char *src_name;
char *dst_name;
int prec_pref_size;
int prec_pat_size;
struct job_prec *prec_pref;
struct job_prec *prec_pat;
};
#endif

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: nonencoded_task_params.h
Author: Unknown
Function:
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/
c_posix_implementation/
Original name: nonencoded_task_params.h
Changes: No major functional changes.
License: See the terms above.
*/
#ifndef _nonencoded_task_params_H
#define _nonencoded_task_params_H
#define NULL ((void*)0)
// Description of a real time task, without precedence encoding.
struct nonencoded_task_params {
char *ne_t_name;
int ne_t_period;
int ne_t_initial_release;
int ne_t_wcet;
int ne_t_deadline;
int ( *ne_t_body )( void * ); // This is the code to execute at each
// instance of the task.
};
#endif

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: ros_th3
Author: Dustin Green and others
Function: executes the third thread of original threads.c
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/c_posix_implementation/
Original name: threads, rosace
Changes: union of rosace.c and threads.c
License: see above
*/
#include "types.h"
#include "assemblage_includes.h"
#include "assemblage.h"
#include "common.h"
// Return variable
int ros_th3_check;
/*
Forward declaration of functions
*/
void* ros_th3_thread3( void* arg );
int ros_th3_run_rosace( uint64_t nbstep );
int main( void );
void ros_th3_init( void );
void ros_th3_main( void );
int ros_th3_return( void );
/*
Initialization function
*/
void ros_th3_init( void )
{
ros_th3_check = -1;
rosace_init();
}
/*
Return function
*/
int ros_th3_return( void )
{
return ros_th3_check;
}
/*
Main functions
*/
void _Pragma( "entrypoint" ) ros_th3_main( void )
{
uint64_t tsimu = 300*200;
ros_th3_check = ros_th3_run_rosace( tsimu );
}
int ros_th3_run_rosace( uint64_t nbstep ){
max_step_simu = nbstep;
// Set first command
ROSACE_update_altitude_command( 11000.0 );
// Exit
ros_th3_thread3( NULL );
return 0;
}
void* ros_th3_thread3( void* arg ) {
uint64_t mystep_simu = step_simu;
_Pragma( "loopbound min 60000 max 60000" )
while( mystep_simu<max_step_simu ) {
// --- 100 Hz ---
if( mystep_simu%2 == 0 ) {
CALL(Q_FILTER);
}
// --- End 100 Hz ---
mystep_simu++;
}
return NULL;
}
int main( void )
{
ros_th3_init();
ros_th3_main();
return ros_th3_return();
}

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/* ----------------------------------------------------------------------------
SchedMCore - A MultiCore Scheduling Framework
Copyright (C) 2009-2011, ONERA, Toulouse, FRANCE - LIFL, Lille, FRANCE
This file is part of Prelude
Prelude is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public License
as published by the Free Software Foundation ; either version 2 of
the License, or (at your option) any later version.
Prelude is distributed in the hope that it will be useful, but
WITHOUT ANY WARRANTY ; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public
License along with this program ; if not, write to the Free Software
Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307
USA
---------------------------------------------------------------------------- */
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: types.h
Author: Unknown
Function:
Source: https://svn.onera.fr/schedmcore/branches/ROSACE_CaseStudy/
c_posix_implementation/
Original name: types.h
Changes: No major functional changes.
License: See the terms above.
*/
#ifndef __DEF_ROSACE_TYPES_H
#define __DEF_ROSACE_TYPES_H
#ifdef USE_FLOAT
#define REAL_TYPE float
#else
#define REAL_TYPE double
#endif
typedef unsigned long long uint64_t;
/* we need forward declaration only in order
* to avoid redefinition in assemblage_vX generated headers
* Real "#include "assemblage.h" is only done in assemblage_includes.c
*/
struct aircraft_dynamics_outs_t {
REAL_TYPE Va;
REAL_TYPE Vz;
REAL_TYPE q;
REAL_TYPE az;
REAL_TYPE h;
};
typedef enum SAMPLE_RANK {
SPL_T, SPL_VA,SPL_AZ,SPL_Q,SPL_VZ,SPL_H,
SPL_DELTA_TH_C, SPL_DELTA_E_C,
SPL_SIZE
} SampleRank_t;
#endif

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/*
====================================================
Copyright (C) 1993 by Sun Microsystems, Inc. All rights reserved.
Developed at SunPro, a Sun Microsystems, Inc. business.
Permission to use, copy, modify, and distribute this
software is freely granted, provided that this notice
is preserved.
====================================================
*/
/*
This program is part of the TACLeBench benchmark suite.
Version V 1.9
Name: wcclibm.h
Author: Unknown
Function: IEEE754 software library routines.
Source: Sun Microsystems
Original name: wcclibm.h
Changes: No major functional changes.
License: See the terms above.
*/
#ifndef _WCCLIBM
#define _WCCLIBM
#define int32_t int
#define u_int32_t unsigned int
// Often used variables/consts
static const float basicmath_one = 1.0f,
basicmath_tiny = 1.0e-30f,
basicmath_half = 5.0000000000e-01, /* 0x3f000000 */
basicmath_huge = 1.0e30,
basicmath_two = 2.0,
basicmath_two24 = 16777216.0, /* 0x4b800000 */
basicmath_zero = 0.0;
#define __ieee754_acosf acosf
#define __atanf atanf
#define __ceilf ceilf
#define __cosf cosf
#define __fabsf fabsf
#define __isinff isinff
#define __ieee754_expf expf
#define __erff erff
#define __ieee754_powf powf
#define __ieee754_sqrtf sqrtf
#define __ieee754_log10f log10f
#define __ieee754_logf logf
#define __sinf sinf
#define __floorf floorf
float __atanf(float x);
float __ceilf(float x);
static float __copysignf(float x, float y);
float __cosf(float x);
float __erff(float x);
float __fabsf(float x);
float __floorf(float x);
float __ieee754_acosf(float x);
float __ieee754_expf(float x);
float __ieee754_logf(float x);
float __ieee754_log10f(float x);
float __ieee754_powf(float x, float y);
static int32_t __ieee754_rem_pio2f(float x, float *y);
float __ieee754_sqrtf(float x);
int __isinff(float x);
static float __kernel_cosf(float x, float y);
static float __kernel_sinf(float x, float y, int iy);
static int __kernel_rem_pio2f(float *x, float *y, int e0, int nx,
int prec, const int32_t *ipio2);
float __sinf(float x);
float __scalbnf(float x, int n);
#endif // _WCCLIBM