548 lines
18 KiB
C
548 lines
18 KiB
C
/* ----------------------------------------------------------------------------
|
|
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;
|
|
}
|