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431 lines
15 KiB
431 lines
15 KiB
#include <stdlib.h>
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#include <stdbool.h>
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#include "assemblage.h"
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#include "assemblage_includes.h"
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double aircraft_dynamics495_Va_Va_filter_100449_Va[2];
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double Vz_control_50483_delta_e_c_elevator489_delta_e_c;
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double Va_filter_100449_Va_f_Va_control_50474_Va_f[2];
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double Vz_filter_100452_Vz_f_Va_control_50474_Vz_f[2];
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double q_filter_100455_q_f_Va_control_50474_q_f[2];
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double Va_c_Va_control_50474_Va_c;
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double h_filter_100446_h_f_altitude_hold_50464_h_f[2];
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double h_c_altitude_hold_50464_h_c;
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double Va_control_50474_delta_th_c_delta_th_c;
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double aircraft_dynamics495_az_az_filter_100458_az[2];
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double aircraft_dynamics495_Vz_Vz_filter_100452_Vz[2];
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double aircraft_dynamics495_q_q_filter_100455_q[2];
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double elevator489_delta_e_aircraft_dynamics495_delta_e[3]={0.0120096156525, 0.0120096156525, 0.0120096156525};
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double engine486_T_aircraft_dynamics495_T[3]={41813.9211946, 41813.9211946, 41813.9211946};
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double aircraft_dynamics495_h_h_filter_100446_h[2];
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double Va_control_50474_delta_th_c_engine486_delta_th_c;
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double Vz_filter_100452_Vz_f_Vz_control_50483_Vz_f[2];
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double altitude_hold_50464_Vz_c_Vz_control_50483_Vz_c;
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double q_filter_100455_q_f_Vz_control_50483_q_f[2];
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double az_filter_100458_az_f_Vz_control_50483_az_f[2];
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double Vz_control_50483_delta_e_c_delta_e_c;
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int Va_filter_100449_fun(void* args)
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{
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double Va_f;
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static int Va_rcell=0;
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const struct write_proto_t Va_f_Va_control_50474_Va_f_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int Va_f_Va_control_50474_Va_f_wcell=0;
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static int instance=0;
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Va_f=Va_filter_100(aircraft_dynamics495_Va_Va_filter_100449_Va[Va_rcell]);
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Va_rcell=(Va_rcell+1)%2;
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if(must_write(Va_f_Va_control_50474_Va_f_write,instance)) {
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Va_filter_100449_Va_f_Va_control_50474_Va_f[Va_f_Va_control_50474_Va_f_wcell]=Va_f;
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Va_f_Va_control_50474_Va_f_wcell=(Va_f_Va_control_50474_Va_f_wcell+1)%2;
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}
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instance++;
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return 0;
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}
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int elevator489_fun(void* args)
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{
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double delta_e;
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static int delta_e_aircraft_dynamics495_delta_e_wcell=1;
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static int instance=0;
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delta_e=elevator(Vz_control_50483_delta_e_c_elevator489_delta_e_c);
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elevator489_delta_e_aircraft_dynamics495_delta_e[delta_e_aircraft_dynamics495_delta_e_wcell]=delta_e;
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delta_e_aircraft_dynamics495_delta_e_wcell=(delta_e_aircraft_dynamics495_delta_e_wcell+1)%3;
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instance++;
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return 0;
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}
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int Va_control_50474_fun(void* args)
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{
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double delta_th_c;
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static int Va_f_rcell=0;
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static int Vz_f_rcell=0;
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static int q_f_rcell=0;
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static int instance=0;
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delta_th_c=Va_control_50(Va_filter_100449_Va_f_Va_control_50474_Va_f[Va_f_rcell],
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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],
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Va_c_Va_control_50474_Va_c);
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Va_f_rcell=(Va_f_rcell+1)%2;
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Vz_f_rcell=(Vz_f_rcell+1)%2;
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q_f_rcell=(q_f_rcell+1)%2;
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Va_control_50474_delta_th_c_engine486_delta_th_c=delta_th_c;
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Va_control_50474_delta_th_c_delta_th_c=delta_th_c;
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instance++;
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return 0;
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}
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int Va_c0_fun(void* args)
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{
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double Va_c;
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static int instance=0;
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Va_c=input_Va_c();
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Va_c_Va_control_50474_Va_c=Va_c;
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instance++;
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return 0;
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}
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int altitude_hold_50464_fun(void* args)
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{
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double Vz_c;
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static int h_f_rcell=0;
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static int instance=0;
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Vz_c=altitude_hold_50(h_filter_100446_h_f_altitude_hold_50464_h_f[h_f_rcell],
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h_c_altitude_hold_50464_h_c);
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h_f_rcell=(h_f_rcell+1)%2;
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altitude_hold_50464_Vz_c_Vz_control_50483_Vz_c=Vz_c;
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instance++;
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return 0;
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}
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int delta_th_c0_fun(void* args)
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{
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static int instance=0;
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output_delta_th_c(Va_control_50474_delta_th_c_delta_th_c);
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instance++;
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return 0;
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}
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int az_filter_100458_fun(void* args)
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{
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double az_f;
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static int az_rcell=0;
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const struct write_proto_t az_f_Vz_control_50483_az_f_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int az_f_Vz_control_50483_az_f_wcell=0;
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static int instance=0;
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az_f=az_filter_100(aircraft_dynamics495_az_az_filter_100458_az[az_rcell]);
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az_rcell=(az_rcell+1)%2;
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if(must_write(az_f_Vz_control_50483_az_f_write,instance)) {
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az_filter_100458_az_f_Vz_control_50483_az_f[az_f_Vz_control_50483_az_f_wcell]=az_f;
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az_f_Vz_control_50483_az_f_wcell=(az_f_Vz_control_50483_az_f_wcell+1)%2;
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}
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instance++;
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return 0;
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}
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int Vz_filter_100452_fun(void* args)
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{
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double Vz_f;
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static int Vz_rcell=0;
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const struct write_proto_t Vz_f_Va_control_50474_Vz_f_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int Vz_f_Va_control_50474_Vz_f_wcell=0;
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const struct write_proto_t Vz_f_Vz_control_50483_Vz_f_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int Vz_f_Vz_control_50483_Vz_f_wcell=0;
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static int instance=0;
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Vz_f=Vz_filter_100(aircraft_dynamics495_Vz_Vz_filter_100452_Vz[Vz_rcell]);
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Vz_rcell=(Vz_rcell+1)%2;
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if(must_write(Vz_f_Va_control_50474_Vz_f_write,instance)) {
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Vz_filter_100452_Vz_f_Va_control_50474_Vz_f[Vz_f_Va_control_50474_Vz_f_wcell]=Vz_f;
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Vz_f_Va_control_50474_Vz_f_wcell=(Vz_f_Va_control_50474_Vz_f_wcell+1)%2;
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}
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if(must_write(Vz_f_Vz_control_50483_Vz_f_write,instance)) {
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Vz_filter_100452_Vz_f_Vz_control_50483_Vz_f[Vz_f_Vz_control_50483_Vz_f_wcell]=Vz_f;
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Vz_f_Vz_control_50483_Vz_f_wcell=(Vz_f_Vz_control_50483_Vz_f_wcell+1)%2;
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}
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instance++;
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return 0;
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}
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int q_filter_100455_fun(void* args)
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{
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double q_f;
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static int q_rcell=0;
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const struct write_proto_t q_f_Va_control_50474_q_f_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int q_f_Va_control_50474_q_f_wcell=0;
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const struct write_proto_t q_f_Vz_control_50483_q_f_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int q_f_Vz_control_50483_q_f_wcell=0;
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static int instance=0;
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q_f=q_filter_100(aircraft_dynamics495_q_q_filter_100455_q[q_rcell]);
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q_rcell=(q_rcell+1)%2;
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if(must_write(q_f_Va_control_50474_q_f_write,instance)) {
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q_filter_100455_q_f_Va_control_50474_q_f[q_f_Va_control_50474_q_f_wcell]=q_f;
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q_f_Va_control_50474_q_f_wcell=(q_f_Va_control_50474_q_f_wcell+1)%2;
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}
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if(must_write(q_f_Vz_control_50483_q_f_write,instance)) {
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q_filter_100455_q_f_Vz_control_50483_q_f[q_f_Vz_control_50483_q_f_wcell]=q_f;
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q_f_Vz_control_50483_q_f_wcell=(q_f_Vz_control_50483_q_f_wcell+1)%2;
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}
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instance++;
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return 0;
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}
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int aircraft_dynamics495_fun(void* args)
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{
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struct aircraft_dynamics_outs_t aircraft_dynamics495_fun_outs;
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static int delta_e_rcell=0;
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static int T_rcell=0;
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const struct write_proto_t Va_Va_filter_100449_Va_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int Va_Va_filter_100449_Va_wcell=0;
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const struct write_proto_t Vz_Vz_filter_100452_Vz_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int Vz_Vz_filter_100452_Vz_wcell=0;
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const struct write_proto_t q_q_filter_100455_q_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int q_q_filter_100455_q_wcell=0;
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const struct write_proto_t az_az_filter_100458_az_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int az_az_filter_100458_az_wcell=0;
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const struct write_proto_t h_h_filter_100446_h_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int h_h_filter_100446_h_wcell=0;
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static int instance=0;
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aircraft_dynamics(elevator489_delta_e_aircraft_dynamics495_delta_e[delta_e_rcell],
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engine486_T_aircraft_dynamics495_T[T_rcell],&aircraft_dynamics495_fun_outs);
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delta_e_rcell=(delta_e_rcell+1)%3;
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T_rcell=(T_rcell+1)%3;
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if(must_write(Va_Va_filter_100449_Va_write,instance)) {
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aircraft_dynamics495_Va_Va_filter_100449_Va[Va_Va_filter_100449_Va_wcell]=aircraft_dynamics495_fun_outs.Va;
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Va_Va_filter_100449_Va_wcell=(Va_Va_filter_100449_Va_wcell+1)%2;
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}
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if(must_write(Vz_Vz_filter_100452_Vz_write,instance)) {
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aircraft_dynamics495_Vz_Vz_filter_100452_Vz[Vz_Vz_filter_100452_Vz_wcell]=aircraft_dynamics495_fun_outs.Vz;
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Vz_Vz_filter_100452_Vz_wcell=(Vz_Vz_filter_100452_Vz_wcell+1)%2;
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}
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if(must_write(q_q_filter_100455_q_write,instance)) {
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aircraft_dynamics495_q_q_filter_100455_q[q_q_filter_100455_q_wcell]=aircraft_dynamics495_fun_outs.q;
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q_q_filter_100455_q_wcell=(q_q_filter_100455_q_wcell+1)%2;
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}
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if(must_write(az_az_filter_100458_az_write,instance)) {
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aircraft_dynamics495_az_az_filter_100458_az[az_az_filter_100458_az_wcell]=aircraft_dynamics495_fun_outs.az;
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az_az_filter_100458_az_wcell=(az_az_filter_100458_az_wcell+1)%2;
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}
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if(must_write(h_h_filter_100446_h_write,instance)) {
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aircraft_dynamics495_h_h_filter_100446_h[h_h_filter_100446_h_wcell]=aircraft_dynamics495_fun_outs.h;
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h_h_filter_100446_h_wcell=(h_h_filter_100446_h_wcell+1)%2;
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}
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instance++;
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return 0;
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}
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int h_filter_100446_fun(void* args)
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{
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double h_f;
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static int h_rcell=0;
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const struct write_proto_t h_f_altitude_hold_50464_h_f_write =
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{ NULL, 0, (int []){ true , false }, 2 };
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static int h_f_altitude_hold_50464_h_f_wcell=0;
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static int instance=0;
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h_f=h_filter_100(aircraft_dynamics495_h_h_filter_100446_h[h_rcell]);
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h_rcell=(h_rcell+1)%2;
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if(must_write(h_f_altitude_hold_50464_h_f_write,instance)) {
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h_filter_100446_h_f_altitude_hold_50464_h_f[h_f_altitude_hold_50464_h_f_wcell]=h_f;
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h_f_altitude_hold_50464_h_f_wcell=(h_f_altitude_hold_50464_h_f_wcell+1)%2;
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}
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instance++;
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return 0;
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}
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int engine486_fun(void* args)
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{
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double T;
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static int T_aircraft_dynamics495_T_wcell=1;
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static int instance=0;
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T=engine(Va_control_50474_delta_th_c_engine486_delta_th_c);
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engine486_T_aircraft_dynamics495_T[T_aircraft_dynamics495_T_wcell]=T;
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T_aircraft_dynamics495_T_wcell=(T_aircraft_dynamics495_T_wcell+1)%3;
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instance++;
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return 0;
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}
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int Vz_control_50483_fun(void* args)
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{
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double delta_e_c;
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static int Vz_f_rcell=0;
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static int q_f_rcell=0;
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static int az_f_rcell=0;
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static int instance=0;
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delta_e_c=Vz_control_50(Vz_filter_100452_Vz_f_Vz_control_50483_Vz_f[Vz_f_rcell],
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altitude_hold_50464_Vz_c_Vz_control_50483_Vz_c,q_filter_100455_q_f_Vz_control_50483_q_f[q_f_rcell],
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az_filter_100458_az_f_Vz_control_50483_az_f[az_f_rcell]);
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Vz_f_rcell=(Vz_f_rcell+1)%2;
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q_f_rcell=(q_f_rcell+1)%2;
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az_f_rcell=(az_f_rcell+1)%2;
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Vz_control_50483_delta_e_c_delta_e_c=delta_e_c;
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Vz_control_50483_delta_e_c_elevator489_delta_e_c=delta_e_c;
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instance++;
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return 0;
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}
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int delta_e_c0_fun(void* args)
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{
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static int instance=0;
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output_delta_e_c(Vz_control_50483_delta_e_c_delta_e_c);
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instance++;
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return 0;
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}
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int h_c0_fun(void* args)
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{
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double h_c;
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static int instance=0;
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h_c=input_h_c();
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h_c_altitude_hold_50464_h_c=h_c;
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instance++;
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return 0;
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}
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#define PLUD_TASK_NUMBER 15
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static struct nonencoded_task_params static_task_set[PLUD_TASK_NUMBER] = {
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{ "h_c0", 1000, 0, 1, 1000, h_c0_fun },
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{ "delta_e_c0", 200, 0, 1, 200, delta_e_c0_fun },
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{ "Vz_control_50483", 200, 0, 1, 200, Vz_control_50483_fun },
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{ "engine486", 50, 0, 1, 50, engine486_fun },
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{ "h_filter_100446", 100, 0, 1, 100, h_filter_100446_fun },
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{ "aircraft_dynamics495", 50, 0, 1, 50, aircraft_dynamics495_fun },
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{ "q_filter_100455", 100, 0, 1, 100, q_filter_100455_fun },
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{ "Vz_filter_100452", 100, 0, 1, 100, Vz_filter_100452_fun },
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{ "az_filter_100458", 100, 0, 1, 100, az_filter_100458_fun },
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{ "delta_th_c0", 200, 0, 1, 200, delta_th_c0_fun },
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{ "altitude_hold_50464", 200, 0, 1, 200, altitude_hold_50464_fun },
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{ "Va_c0", 1000, 0, 1, 1000, Va_c0_fun },
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{ "Va_control_50474", 200, 0, 1, 200, Va_control_50474_fun },
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{ "elevator489", 50, 0, 1, 50, elevator489_fun },
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{ "Va_filter_100449", 100, 0, 1, 100, Va_filter_100449_fun }
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};
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void get_task_set (int* task_number, struct nonencoded_task_params** task_set)
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{
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*task_number = PLUD_TASK_NUMBER;
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*task_set=static_task_set;
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}
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static struct job_prec engine486_aircraft_dynamics495_pcpat[1] = { {0,1} };
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static struct job_prec Va_filter_100449_Va_control_50474_pcpat[1] = {
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{0,0} };
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static struct job_prec q_filter_100455_Va_control_50474_pcpat[1] = { {0,0} };
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static struct job_prec q_filter_100455_Vz_control_50483_pcpat[1] = { {0,0} };
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static struct job_prec aircraft_dynamics495_q_filter_100455_pcpat[1] = {
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{0,0} };
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static struct job_prec Va_c0_Va_control_50474_pcpat[1] = { {0,0} };
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static struct job_prec Vz_control_50483_delta_e_c0_pcpat[1] = { {0,0} };
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static struct job_prec Vz_control_50483_elevator489_pcpat[1] = { {0,0} };
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static struct job_prec Vz_filter_100452_Va_control_50474_pcpat[1] = {
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{0,0} };
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static struct job_prec Vz_filter_100452_Vz_control_50483_pcpat[1] = {
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{0,0} };
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static struct job_prec h_filter_100446_altitude_hold_50464_pcpat[1] = {
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{0,0} };
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static struct job_prec aircraft_dynamics495_az_filter_100458_pcpat[1] = {
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{0,0} };
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static struct job_prec elevator489_aircraft_dynamics495_pcpat[1] = { {0,1} };
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static struct job_prec aircraft_dynamics495_Vz_filter_100452_pcpat[1] = {
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{0,0} };
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static struct job_prec az_filter_100458_Vz_control_50483_pcpat[1] = {
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{0,0} };
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static struct job_prec h_c0_altitude_hold_50464_pcpat[1] = { {0,0} };
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static struct job_prec altitude_hold_50464_Vz_control_50483_pcpat[1] = {
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{0,0} };
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static struct job_prec aircraft_dynamics495_Va_filter_100449_pcpat[1] = {
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|
{0,0} };
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static struct job_prec aircraft_dynamics495_h_filter_100446_pcpat[1] = {
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{0,0} };
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static struct job_prec Va_control_50474_engine486_pcpat[1] = { {0,0} };
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static struct job_prec Va_control_50474_delta_th_c0_pcpat[1] = { {0,0} };
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|
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#define PLUD_PREC_NUMBER 21
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static struct multirate_precedence static_prec_set[PLUD_PREC_NUMBER] = {
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{ "engine486", "aircraft_dynamics495", 0, 1, NULL,
|
|
engine486_aircraft_dynamics495_pcpat },
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|
{ "Va_filter_100449", "Va_control_50474", 0, 1, NULL,
|
|
Va_filter_100449_Va_control_50474_pcpat },
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|
{ "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 },
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|
{ "aircraft_dynamics495", "q_filter_100455", 0, 1, NULL,
|
|
aircraft_dynamics495_q_filter_100455_pcpat },
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|
{ "Va_c0", "Va_control_50474", 0, 1, NULL, Va_c0_Va_control_50474_pcpat },
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|
{ "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;
|
|
}
|