uiuc_warnings_errors.cpp uiuc_warnings_errors.h \
uiuc_wrapper.cpp uiuc_wrapper.h
-INCLUDES += -I$(top_srcdir)
+INCLUDES += -I$(top_srcdir) -I$(top_srcdir)/src
#define _AERODEFLECTIONS_H_
#include "uiuc_aircraft.h" /* aileron, elevator, rudder */
-#include "../LaRCsim/ls_cockpit.h" /* Long_control, Lat_control, Rudder_pedal */
-#include "../LaRCsim/ls_constants.h" /* RAD_TO_DEG, DEG_TO_RAD */
+#include <FDM/LaRCsim/ls_cockpit.h> /* Long_control, Lat_control, Rudder_pedal */
+#include <FDM/LaRCsim/ls_constants.h> /* RAD_TO_DEG, DEG_TO_RAD */
void uiuc_aerodeflections( double dt );
#ifndef _BETAPROBE_H_
#define _BETAPROBE_H_
-#include "uiuc_aircraft.h"
-#include "../FDM/LaRCsim/ls_constants.h"
-#include "../FDM/LaRCsim/ls_generic.h"
#include <math.h>
+#include <FDM/LaRCsim/ls_constants.h>
+#include <FDM/LaRCsim/ls_generic.h>
+
+#include "uiuc_aircraft.h"
+
void uiuc_betaprobe();
#endif // _BETAPROBE_H_
#ifndef _COEF_DRAG_H_
#define _COEF_DRAG_H_
+#include <FDM/LaRCsim/ls_generic.h>
+
#include "uiuc_parsefile.h"
#include "uiuc_aircraft.h"
#include "uiuc_1Dinterpolation.h"
#include "uiuc_2Dinterpolation.h"
#include "uiuc_ice.h"
-#include "../FDM/LaRCsim/ls_generic.h"
void uiuc_coef_drag();
#ifndef _COEF_LIFT_H_
#define _COEF_LIFT_H_
+#include <FDM/LaRCsim/ls_generic.h>
+
#include "uiuc_parsefile.h"
#include "uiuc_aircraft.h"
#include "uiuc_1Dinterpolation.h"
#include "uiuc_2Dinterpolation.h"
#include "uiuc_ice.h"
-#include "../FDM/LaRCsim/ls_generic.h"
void uiuc_coef_lift();
#include "uiuc_1Dinterpolation.h"
#include "uiuc_2Dinterpolation.h"
#include "uiuc_ice.h"
-#include "../FDM/LaRCsim/ls_generic.h"
+#include <FDM/LaRCsim/ls_generic.h>
void uiuc_coef_pitch();
#include "uiuc_1Dinterpolation.h"
#include "uiuc_2Dinterpolation.h"
#include "uiuc_ice.h"
-#include "../FDM/LaRCsim/ls_generic.h"
+#include <FDM/LaRCsim/ls_generic.h>
void uiuc_coef_roll();
#include "uiuc_1Dinterpolation.h"
#include "uiuc_2Dinterpolation.h"
#include "uiuc_ice.h"
-#include "../FDM/LaRCsim/ls_generic.h"
+#include <FDM/LaRCsim/ls_generic.h>
void uiuc_coef_sideforce();
#include "uiuc_1Dinterpolation.h"
#include "uiuc_2Dinterpolation.h"
#include "uiuc_ice.h"
-#include "../FDM/LaRCsim/ls_generic.h"
+#include <FDM/LaRCsim/ls_generic.h>
void uiuc_coef_yaw();
#include "uiuc_coef_sideforce.h"
#include "uiuc_coef_roll.h"
#include "uiuc_coef_yaw.h"
-#include "../LaRCsim/ls_generic.h"
+#include <FDM/LaRCsim/ls_generic.h>
void uiuc_coefficients();
#ifndef _CONVERT_H_
#define _CONVERT_H_
-#include "../LaRCsim/ls_constants.h" /* uses RAD_TO_DEG, DEG_TO_RAD */
+#include <FDM/LaRCsim/ls_constants.h> /* uses RAD_TO_DEG, DEG_TO_RAD */
double uiuc_convert( int conversionType );
#define _ENGINE_H_
#include "uiuc_aircraft.h"
-#include "../LaRCsim/ls_generic.h"
-#include "../LaRCsim/ls_cockpit.h"
+#include <FDM/LaRCsim/ls_generic.h>
+#include <FDM/LaRCsim/ls_cockpit.h>
void uiuc_engine();
#endif // _ENGINE_H_
#include "uiuc_initializemaps.h"
#include "uiuc_1DdataFileReader.h"
#include "uiuc_2DdataFileReader.h"
-#include "../FDM/LaRCsim/ls_generic.h"
-#include "../FDM/LaRCsim/ls_cockpit.h" /* Long_trim defined */
-#include "../FDM/LaRCsim/ls_constants.h" /* INVG defined */
+#include <FDM/LaRCsim/ls_generic.h>
+#include <FDM/LaRCsim/ls_cockpit.h> /* Long_trim defined */
+#include <FDM/LaRCsim/ls_constants.h> /* INVG defined */
bool check_float(string &token); // To check whether the token is a float or not
void uiuc_menu (string aircraft);
#include "uiuc_parsefile.h"
#include "uiuc_aircraft.h"
-#include "../FDM/LaRCsim/ls_generic.h"
-#include "../FDM/LaRCsim/ls_cockpit.h"
-#include "../FDM/LaRCsim/ls_constants.h"
+#include <FDM/LaRCsim/ls_generic.h>
+#include <FDM/LaRCsim/ls_cockpit.h>
+#include <FDM/LaRCsim/ls_constants.h>
extern double Simtime;
#include "uiuc_recorder.h"
#include "uiuc_menu.h"
#include "uiuc_betaprobe.h"
-#include "../FDM/LaRCsim/ls_generic.h"
+#include <FDM/LaRCsim/ls_generic.h>
extern "C" void uiuc_init_aeromodel ();
extern "C" void uiuc_force_moment(double dt);