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