/********************************************************************** FILENAME: uiuc_icing_demo.cpp ---------------------------------------------------------------------- DESCRIPTION: ---------------------------------------------------------------------- STATUS: alpha version ---------------------------------------------------------------------- REFERENCES: ---------------------------------------------------------------------- HISTORY: 12/02/2002 initial release - originally in uiuc_coefficients() ---------------------------------------------------------------------- AUTHOR(S): Robert Deters ---------------------------------------------------------------------- VARIABLES: ---------------------------------------------------------------------- INPUTS: ---------------------------------------------------------------------- OUTPUTS: ---------------------------------------------------------------------- CALLED BY: uiuc_coefficients ---------------------------------------------------------------------- CALLS TO: ---------------------------------------------------------------------- COPYRIGHT: (C) 2002 by Michael Selig This program is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation. This program 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 General Public License for more details. You should have received a copy of the GNU 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 or view http://www.gnu.org/copyleft/gpl.html. **********************************************************************/ #include "uiuc_icing_demo.h" void uiuc_icing_demo() { // Envelope protection values if (demo_eps_alpha_max) { double time = Simtime - demo_eps_alpha_max_startTime; eps_alpha_max = uiuc_1Dinterpolation(demo_eps_alpha_max_timeArray, demo_eps_alpha_max_daArray, demo_eps_alpha_max_ntime, time); } if (demo_eps_pitch_max) { double time = Simtime - demo_eps_pitch_max_startTime; eps_pitch_max = uiuc_1Dinterpolation(demo_eps_pitch_max_timeArray, demo_eps_pitch_max_daArray, demo_eps_pitch_max_ntime, time); } if (demo_eps_pitch_min) { double time = Simtime - demo_eps_pitch_min_startTime; eps_pitch_min = uiuc_1Dinterpolation(demo_eps_pitch_min_timeArray, demo_eps_pitch_min_daArray, demo_eps_pitch_min_ntime, time); } if (demo_eps_roll_max) { double time = Simtime - demo_eps_roll_max_startTime; eps_roll_max = uiuc_1Dinterpolation(demo_eps_roll_max_timeArray, demo_eps_roll_max_daArray, demo_eps_roll_max_ntime, time); } if (demo_eps_thrust_min) { double time = Simtime - demo_eps_thrust_min_startTime; eps_thrust_min = uiuc_1Dinterpolation(demo_eps_thrust_min_timeArray, demo_eps_thrust_min_daArray, demo_eps_thrust_min_ntime, time); } if (demo_eps_airspeed_max) { double time = Simtime - demo_eps_airspeed_max_startTime; eps_airspeed_max = uiuc_1Dinterpolation(demo_eps_airspeed_max_timeArray, demo_eps_airspeed_max_daArray, demo_eps_airspeed_max_ntime, time); } if (demo_eps_airspeed_min) { double time = Simtime - demo_eps_airspeed_min_startTime; eps_airspeed_min = uiuc_1Dinterpolation(demo_eps_airspeed_min_timeArray, demo_eps_airspeed_min_daArray, demo_eps_airspeed_min_ntime, time); } if (demo_eps_flap_max) { double time = Simtime - demo_eps_flap_max_startTime; eps_flap_max = uiuc_1Dinterpolation(demo_eps_flap_max_timeArray, demo_eps_flap_max_daArray, demo_eps_flap_max_ntime, time); } if (demo_eps_pitch_input) { double time = Simtime - demo_eps_pitch_input_startTime; eps_pitch_input = uiuc_1Dinterpolation(demo_eps_pitch_input_timeArray, demo_eps_pitch_input_daArray, demo_eps_pitch_input_ntime, time); } // Boot cycle values if (demo_boot_cycle_tail) { double time = Simtime - demo_boot_cycle_tail_startTime; boot_cycle_tail = uiuc_1Dinterpolation(demo_boot_cycle_tail_timeArray, demo_boot_cycle_tail_daArray, demo_boot_cycle_tail_ntime, time); } if (demo_boot_cycle_wing_left) { double time = Simtime - demo_boot_cycle_wing_left_startTime; boot_cycle_wing_left = uiuc_1Dinterpolation(demo_boot_cycle_wing_left_timeArray, demo_boot_cycle_wing_left_daArray, demo_boot_cycle_wing_left_ntime, time); } if (demo_boot_cycle_wing_right) { double time = Simtime - demo_boot_cycle_wing_right_startTime; boot_cycle_wing_right = uiuc_1Dinterpolation(demo_boot_cycle_wing_right_timeArray, demo_boot_cycle_wing_right_daArray, demo_boot_cycle_wing_right_ntime, time); } // Ice values if (demo_ice_tail) { double time = Simtime - demo_ice_tail_startTime; ice_tail = uiuc_1Dinterpolation(demo_ice_tail_timeArray, demo_ice_tail_daArray, demo_ice_tail_ntime, time); } if (demo_ice_left) { double time = Simtime - demo_ice_left_startTime; ice_left = uiuc_1Dinterpolation(demo_ice_left_timeArray, demo_ice_left_daArray, demo_ice_left_ntime, time); } if (demo_ice_right) { double time = Simtime - demo_ice_right_startTime; ice_right = uiuc_1Dinterpolation(demo_ice_right_timeArray, demo_ice_right_daArray, demo_ice_right_ntime, time); } // Autopilot if (demo_ap_pah_on){ double time = Simtime - demo_ap_pah_on_startTime; ap_pah_on = uiuc_1Dinterpolation(demo_ap_pah_on_timeArray, demo_ap_pah_on_daArray, demo_ap_pah_on_ntime, time); } if (demo_ap_Theta_ref_deg){ double time = Simtime - demo_ap_Theta_ref_deg_startTime; ap_Theta_ref_deg = uiuc_1Dinterpolation(demo_ap_Theta_ref_deg_timeArray, demo_ap_Theta_ref_deg_daArray, demo_ap_Theta_ref_deg_ntime, time); } return; }