02/24/2002 (GD) Added uiuc_network_routine()
03/27/2002 (RD) Changed how forces are calculated when
body-axis is used
-
+ 12/11/2002 (RD) Divided uiuc_network_routine into
+ uiuc_network_recv_routine and
+ uiuc_network_send_routine
+ 03/16/2003 (RD) Added trigger lines in recorder area
+
----------------------------------------------------------------------
AUTHOR(S): Bipin Sehgal <bsehgal@uiuc.edu>
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.
-
+ Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA.
+
**********************************************************************/
+#ifdef HAVE_CONFIG_H
+# include <config.h>
+#endif
+
+#include <iostream>
+#include <cstring>
+
#include <simgear/compiler.h>
#include <simgear/misc/sg_path.hxx>
-#include <Aircraft/aircraft.hxx>
#include <Main/fg_props.hxx>
#include "uiuc_aircraft.h"
-#include "uiuc_aircraftdir.h"
#include "uiuc_coefficients.h"
+#include "uiuc_getwind.h"
#include "uiuc_engine.h"
#include "uiuc_gear.h"
#include "uiuc_aerodeflections.h"
//#include "Main/simple_udp.h"
#include "uiuc_fog.h" //321654
//#include "uiuc_network.h"
-//#include "uiuc_get_flapper.h"
-
-#if !defined (SG_HAVE_NATIVE_SGI_COMPILERS)
-SG_USING_STD(cout);
-SG_USING_STD(endl);
-#endif
+#include "uiuc_get_flapper.h"
+extern "C" void uiuc_initial_init ();
+extern "C" void uiuc_defaults_inits ();
+extern "C" void uiuc_vel_init ();
extern "C" void uiuc_init_aeromodel ();
extern "C" void uiuc_force_moment(double dt);
extern "C" void uiuc_engine_routine();
+extern "C" void uiuc_wind_routine();
extern "C" void uiuc_gear_routine();
extern "C" void uiuc_record_routine(double dt);
-//extern "C" void uiuc_network_routine();
-extern "C" void uiuc_vel_init ();
-extern "C" void uiuc_initial_init ();
+extern "C" void uiuc_network_recv_routine();
+extern "C" void uiuc_network_send_routine();
-AIRCRAFT *aircraft_ = new AIRCRAFT;
-AIRCRAFTDIR *aircraftdir_ = new AIRCRAFTDIR;
+AIRCRAFT *aircraft_ = 0;
// SendArray testarray(4950);
void uiuc_initial_init ()
{
+ // This function is called from uiuc_init_2_wrapper (uiuc_aero.c in LaRCsim)
+ // which is called from ls_step and ls_model.
+ // Apply brute force initializations, which override unwanted changes
+ // performed by LaRCsim.
+ // Used during initialization (while Simtime=0).
if (P_body_init_true)
P_body = P_body_init;
if (Q_body_init_true)
V_body = V_body_init;
if (W_body_init_true)
W_body = W_body_init;
+}
+
+void uiuc_defaults_inits ()
+{
+ if (aircraft_ == 0)
+ aircraft_ = new AIRCRAFT;
+
+ // set defaults and initialize (called once from uiuc_init_2_wrapper)
+
+ //fog inits
+ fog_field = 0;
+ fog_segments = 0;
+ fog_point_index = -1;
+ fog_time = NULL;
+ fog_value = NULL;
+ fog_next_time = 0.0;
+ fog_current_segment = 0;
+ Fog = 0;
+
+ use_V_rel_wind_2U = false;
+ nondim_rate_V_rel_wind = false;
+ use_abs_U_body_2U = false;
+ use_dyn_on_speed_curve1 = false;
+ use_Alpha_dot_on_speed = false;
+ use_gamma_horiz_on_speed = false;
+ b_downwashMode = false;
+ P_body_init_true = false;
+ Q_body_init_true = false;
+ R_body_init_true = false;
+ Phi_init_true = false;
+ Theta_init_true = false;
+ Psi_init_true = false;
+ Alpha_init_true = false;
+ Beta_init_true = false;
+ U_body_init_true = false;
+ V_body_init_true = false;
+ W_body_init_true = false;
+ trim_case_2 = false;
+ use_uiuc_network = false;
+ icing_demo = false;
+ outside_control = false;
+ set_Long_trim = false;
+ zero_Long_trim = false;
+ elevator_step = false;
+ elevator_singlet = false;
+ elevator_doublet = false;
+ elevator_input = false;
+ elevator_input_ntime = 0;
+ aileron_input = false;
+ aileron_input_ntime = 0;
+ rudder_input = false;
+ rudder_input_ntime = 0;
+ pilot_elev_no = false;
+ pilot_elev_no_check = false;
+ pilot_ail_no = false;
+ pilot_ail_no_check = false;
+ pilot_rud_no = false;
+ pilot_rud_no_check = false;
+ use_flaps = false;
+ use_spoilers = false;
+ flap_pos_input = false;
+ flap_pos_input_ntime = 0;
+ use_elevator_sas_type1 = false;
+ use_elevator_sas_max = false;
+ use_elevator_sas_min = false;
+ use_elevator_stick_gain = false;
+ use_aileron_sas_type1 = false;
+ use_aileron_sas_max = false;
+ use_aileron_stick_gain = false;
+ use_rudder_sas_type1 = false;
+ use_rudder_sas_max = false;
+ use_rudder_stick_gain = false;
+ simpleSingleModel = false;
+ Throttle_pct_input = false;
+ Throttle_pct_input_ntime = 0;
+ gyroForce_Q_body = false;
+ gyroForce_R_body = false;
+ b_slipstreamEffects = false;
+ Xp_input = false;
+ Xp_input_ntime = 0;
+ Zp_input = false;
+ Zp_input_ntime = 0;
+ Mp_input = false;
+ Mp_input_ntime = 0;
+ b_CLK = false;
+ // gear_model[MAX_GEAR]
+ memset(gear_model,false,MAX_GEAR*sizeof(gear_model[0]));
+ use_gear = false;
+ // start with gear down if it is ultimately used
+ gear_pos_norm = 1;
+ ice_model = false;
+ ice_on = false;
+ beta_model = false;
+ // bootTrue[20] = 0;
+ memset(bootTrue,false,20*sizeof(gear_model[0]));
+ eta_from_file = false;
+ eta_wing_left_input = false;
+ eta_wing_right_input = false;
+ eta_tail_input = false;
+ demo_eps_alpha_max = false;
+ demo_eps_pitch_max = false;
+ demo_eps_pitch_min = false;
+ demo_eps_roll_max = false;
+ demo_eps_thrust_min = false;
+ demo_eps_airspeed_max = false;
+ demo_eps_airspeed_min = false;
+ demo_eps_flap_max = false;
+ demo_boot_cycle_tail = false;
+ demo_boot_cycle_wing_left = false;
+ demo_boot_cycle_wing_right = false;
+ demo_eps_pitch_input = false;
+ tactilefadef = false;
+ demo_ap_pah_on = false;
+ demo_ap_alh_on = false;
+ demo_ap_Theta_ref = false;
+ demo_ap_alt_ref = false;
+ demo_tactile = false;
+ demo_ice_tail = false;
+ demo_ice_left = false;
+ demo_ice_right = false;
+ flapper_model = false;
+ ignore_unknown_keywords = false;
+ pilot_throttle_no = false;
+ Dx_cg = 0.0;
+ Dy_cg = 0.0;
+ Dz_cg = 0.0;
+ ap_pah_on = 0;
+ ap_alh_on = 0;
}
void uiuc_vel_init ()
{
+ // Calculates the local velocity (V_north, V_east, V_down) from the body
+ // velocities.
+ // Called from uiuc_local_vel_init which is called from ls_step.
+ // Used during initialization (while Simtime=0)
if (U_body_init_true && V_body_init_true && W_body_init_true)
{
double det_T_l_to_b, cof11, cof12, cof13, cof21, cof22, cof23, cof31, cof32, cof33;
void uiuc_init_aeromodel ()
{
+ // Initializes the UIUC aircraft model.
+ // Called once from uiuc_init_2_wrapper
SGPath path(globals->get_fg_root());
- path.append(aircraft_dir);
+ path.append(fgGetString("/sim/aircraft-dir"));
path.append("aircraft.dat");
- cout << "We are using "<< path.str() << endl;
+ std::cout << "We are using "<< path.str() << std::endl;
uiuc_initializemaps(); // Initialize the <string,int> maps
uiuc_menu(path.str()); // Read the specified aircraft file
}
uiuc_aerodeflections(dt);
uiuc_coefficients(dt);
- //if (flapper_model)
- // {
- // uiuc_get_flapper(dt);
- // }
/* Calculate the forces */
if (CX && CZ)
if (I_zz_appMass_ratio)
M_n_aero += -(I_zz_appMass_ratio * I_zz) * R_dot_body;
+ // adding in apparent mass in body axis X direction
+ // F_X_aero += -(0.05 * Mass) * U_dot_body;
+
+
if (Mass_appMass)
F_Z_aero += -Mass_appMass * W_dot_body;
if (I_xx_appMass)
M_m_aero += -polarInertia * engineOmega * R_body;
// ornithopter support
- //if (flapper_model)
- // {
- // F_X_aero += F_X_aero_flapper;
- // F_Z_aero += F_Z_aero_flapper;
- // M_m_aero += flapper_Moment;
- // }
+ if (flapper_model)
+ {
+ uiuc_get_flapper(dt);
+ F_X_aero += F_X_aero_flapper;
+ F_Z_aero += F_Z_aero_flapper;
+ M_m_aero += flapper_Moment;
+ }
// fog field update
Fog = 0;
}
+void uiuc_wind_routine()
+{
+ uiuc_getwind();
+}
+
void uiuc_engine_routine()
{
uiuc_engine();
void uiuc_record_routine(double dt)
{
+ if (trigger_last_time_step == 0 && trigger_on == 1) {
+ if (trigger_toggle == 0)
+ trigger_toggle = 1;
+ else
+ trigger_toggle = 0;
+ trigger_num++;
+ if (trigger_num % 2 != 0)
+ trigger_counter++;
+ }
+
if (Simtime >= recordStartTime)
uiuc_recorder(dt);
+
+ trigger_last_time_step = trigger_on;
}
-//void uiuc_network_routine()
-//{
-// if (use_uiuc_network)
-// uiuc_network(2); //send data
-//}
+void uiuc_network_recv_routine()
+{
+ //if (use_uiuc_network)
+ // uiuc_network(1);
+}
+
+void uiuc_network_send_routine()
+{
+ //if (use_uiuc_network)
+ // uiuc_network(2);
+}
//end uiuc_wrapper.cpp
projects / flightgear.git / blobdiff