Exemplo n.º 1
0
/*---------------------------------------------------------------------------------------------------------------------
Navdata handling function, which is called every time navdata are received
---------------------------------------------------------------------------------------------------------------------*/
inline C_RESULT demo_navdata_client_process( const navdata_unpacked_t* const navdata )
{
	static int cpt=0;

    const navdata_demo_t* const nd = &navdata->navdata_demo;


		/**	======= INSERT USER CODE HERE ========== **/
				ARWin32Demo_AcquireConsole();
				if ((cpt++)==90) { system("cls"); cpt=0; }
				
				ARWin32Demo_SetConsoleCursor(0,0);  // Print at the top of the console
				printf("=================================\n");
				printf("Navdata for flight demonstrations\n");
				printf("=================================\n");

				printf("Control state : %s                                      \n",ctrl_state_str(nd->ctrl_state));
				printf("Battery level : %i/100          \n",nd->vbat_flying_percentage);
				printf("Orientation   : [Theta] %4.3f  [Phi] %4.3f  [Psi] %4.3f          \n",nd->theta,nd->phi,nd->psi);
				printf("Altitude      : %i          \n",nd->altitude);
				printf("Speed         : [vX] %4.3f  [vY] %4.3f  [vZ] %4.3f          \n",nd->vx,nd->vy,nd->vz);
				ARWin32Demo_ReleaseConsole();

		/** ======= INSERT USER CODE HERE ========== **/

		return C_OK;
}
Exemplo n.º 2
0
/* Receving navdata during the event loop */
C_RESULT demo_navdata_client_process( const navdata_unpacked_t* const navdata )
{
	static int cpt=0;

	return C_OK;

	const navdata_demo_t*nd = &navdata->navdata_demo;
	const navdata_vision_detect_t*nv = &navdata->navdata_vision_detect;

	printf("==========================\nNavdata for flight demonstrations \n==========================\n");

	printf("Control state : %s\n",ctrl_state_str(nd->ctrl_state));
	printf("Battery level : %i %%\n",nd->vbat_flying_percentage);
	printf("Orientation   : [Theta] %4.3f  [Phi] %4.3f  [Psi] %4.3f\n",nd->theta,nd->phi,nd->psi);
	printf("Altitude      : %i\n",nd->altitude);
	printf("Speed         : [vX] %4.3f  [vY] %4.3f  [vZPsi] %4.3f\n",nd->vx,nd->vy,nd->vz);
	printf("Position      : [x] %4.3f [Y] %4.3f [Z] %4.3f\n",
							nd->drone_camera_trans.x,
							nd->drone_camera_trans.y,
							nd->drone_camera_trans.z);

	printf("Detec. trans. : [x] %4.3f [Y] %4.3f [Z] %4.3f\n",
								nd->detection_camera_trans.x,
								nd->detection_camera_trans.y,
								nd->detection_camera_trans.z);

	printf("Orientation   :\n%4.3f | %4.3f | %4.3f\n%4.3f | %4.3f | %4.3f\n%4.3f | %4.3f | %4.3f\n",
								nd->drone_camera_rot.m11,nd->drone_camera_rot.m12,nd->drone_camera_rot.m13,
								nd->drone_camera_rot.m21,nd->drone_camera_rot.m22,nd->drone_camera_rot.m23,
								nd->drone_camera_rot.m31,nd->drone_camera_rot.m32,nd->drone_camera_rot.m33 );

	printf("Detec. rot.   :\n%4.3f | %4.3f | %4.3f\n%4.3f | %4.3f | %4.3f\n%4.3f | %4.3f | %4.3f\n",
								nd->detection_camera_rot.m11,nd->detection_camera_rot.m12,nd->detection_camera_rot.m13,
								nd->detection_camera_rot.m21,nd->detection_camera_rot.m22,nd->detection_camera_rot.m23,
								nd->detection_camera_rot.m31,nd->detection_camera_rot.m32,nd->detection_camera_rot.m33 );


	printf("=====================\nNavdata for detection \n=====================\n");
	printf("Type     :  %i\n",nd->detection_camera_type);
	printf("Tag index:  %i\n",nd->detection_tag_index);
	printf("Targets  :  %i\n",nv->nb_detected);
	printf("Target 1 :  [X] %4i    [Y] %4i\n",nv->xc[0],nv->yc[0]);
	printf("Target 2 :  [X] %4i    [Y] %4i\n",nv->xc[1],nv->yc[1]);

	printf("\033[27A");

	if ((cpt++)==100)
	  {
	    cpt=system("clear"); // Avoid compiler warning (unused return value)
	    cpt=0;
	  }

  return C_OK;
}
Exemplo n.º 3
0
/**
  * Navdata handling callback
  * This callback is registered to ARDroneTool in the BEGIN_NAVDATA_HANDLER_TABLE in navdata_client.c
  * @param pnd Pointer to the ready-to-use navdata structure
  * @return Always returns C_OK.
  */
C_RESULT navdata_ihm_process( const navdata_unpacked_t* const pnd )
{
  //char text_buffer[1024];
  const navdata_vision_detect_t* pndvision = &pnd->navdata_vision_detect;

  gdk_threads_enter();

  // States' display update for IHM
  vp_os_memset( label_mykonos_state_value, '\0', sizeof(label_mykonos_state_value) );
  sprintf(label_mykonos_state_value, "%08x", pnd->ardrone_state);

  strcpy(label_ctrl_state_value, ctrl_state_str( pnd->navdata_demo.ctrl_state ));
  set_control_state(pnd->navdata_demo.ctrl_state);

  ihm_val_idx--;
  if (ihm_val_idx < 0) ihm_val_idx = KIHM_N_PT2PLOT-1;

  // Angular rates received and displayed in deg/s

  ihm_CA[KIHM_CURVE_GYRO].tval[0][ihm_val_idx] = ((double) pnd->navdata_phys_measures.phys_gyros[GYRO_X]);
  ihm_CA[KIHM_CURVE_GYRO].tval[1][ihm_val_idx] = ((double) pnd->navdata_phys_measures.phys_gyros[GYRO_Y]);
  ihm_CA[KIHM_CURVE_GYRO].tval[2][ihm_val_idx] = ((double) pnd->navdata_phys_measures.phys_gyros[GYRO_Z]);

  // Accelerations are received in mg
  // They are displayed in g: conversion gain is 1/1000
  ihm_CA[KIHM_CURVE_ACC].tval[0][ihm_val_idx] = ((double) pnd->navdata_phys_measures.phys_accs[ACC_X]) / KIHM_MIL_F;
  ihm_CA[KIHM_CURVE_ACC].tval[1][ihm_val_idx] = ((double) pnd->navdata_phys_measures.phys_accs[ACC_Y]) / KIHM_MIL_F;
  ihm_CA[KIHM_CURVE_ACC].tval[2][ihm_val_idx] = ((double) pnd->navdata_phys_measures.phys_accs[ACC_Z]) / KIHM_MIL_F;

  // Filtered  temperature is drawn in the Vbat window
  ihm_CA[KIHM_CURVE_VBAT].tval[0][ihm_val_idx] = ((double) (pnd->navdata_phys_measures.accs_temp));   // Filtered temperature

  ihm_CA[KIHM_CURVE_VBAT].tval[1][ihm_val_idx] = ((double) (pnd->navdata_demo.vbat_flying_percentage)) ; // Filtered vbat in %

  ihm_CA[KIHM_CURVE_THETA].tval[2][ihm_val_idx] = ((double) pnd->navdata_euler_angles.theta_a) / KIHM_MIL_F; // theta accelerometer value
  ihm_CA[KIHM_CURVE_PHI  ].tval[2][ihm_val_idx] = ((double) pnd->navdata_euler_angles.phi_a) / KIHM_MIL_F; // phi accelerometer value

  ihm_CA[KIHM_CURVE_THETA].tval[0][ihm_val_idx] = ((double) pnd->navdata_demo.theta) / KIHM_MIL_F; // theta fused value
  ihm_CA[KIHM_CURVE_PHI  ].tval[0][ihm_val_idx] = ((double) pnd->navdata_demo.phi) / KIHM_MIL_F; // phi fused value
  ihm_psi                                       = ((double) pnd->navdata_demo.psi) / KIHM_MIL_F;

  earef.theta = pnd->navdata_references.ref_theta;
  ihm_CA[KIHM_CURVE_THETA].tval[1][ihm_val_idx] = ((double) earef.theta) / KIHM_MIL_F; // theta reference value

  earef.phi = pnd->navdata_references.ref_phi;
  ihm_CA[KIHM_CURVE_PHI  ].tval[1][ihm_val_idx] = ((double) earef.phi) / KIHM_MIL_F; // phi reference value

  earef.psi = pnd->navdata_references.ref_psi;

  wref.p = pnd->navdata_references.ref_roll;
  wref.q = pnd->navdata_references.ref_pitch;
  wref.r = pnd->navdata_references.ref_yaw;

  rc_ref_gaz = pnd->navdata_rc_references.rc_ref_gaz;

  ihm_CA[KIHM_CURVE_ALTITUDE].tval[0][ihm_val_idx] = ((double) pnd->navdata_demo.altitude);

  ihm_CA[KIHM_CURVE_ALTITUDE].tval[1][ihm_val_idx] = ((double) pnd->navdata_altitude.altitude_vision);
  ihm_CA[KIHM_CURVE_ALTITUDE].tval[2][ihm_val_idx] = ((double) pnd->navdata_altitude.altitude_ref);
  ihm_CA[KIHM_CURVE_ALTITUDE].tval[3][ihm_val_idx] = ((double) pnd->navdata_altitude.altitude_raw);

  ihm_CA[KIHM_CURVE_VZ].tval[1][ihm_val_idx] = (double) (pnd->navdata_altitude.altitude_vz);      // Fusion Vz

  tab_trims[0] = (double)pnd->navdata_trims.euler_angles_trim_theta;
  tab_trims[1] = (double)pnd->navdata_trims.euler_angles_trim_phi;
  tab_trims[2] = (double)pnd->navdata_trims.angular_rates_trim_r;

  ihm_CA[KIHM_CURVE_PWM].tval[0][ihm_val_idx] = (double) (pnd->navdata_pwm.motor1); // PWM motor 1
  ihm_CA[KIHM_CURVE_PWM].tval[1][ihm_val_idx] = (double) (pnd->navdata_pwm.motor2); // PWM motor 2
  ihm_CA[KIHM_CURVE_PWM].tval[2][ihm_val_idx] = (double) (pnd->navdata_pwm.motor3); // PWM motor 3
  ihm_CA[KIHM_CURVE_PWM].tval[3][ihm_val_idx] = (double) (pnd->navdata_pwm.motor4); // PWM motor 4
  ihm_CA[KIHM_CURVE_CURRENT].tval[0][ihm_val_idx] = (double) (pnd->navdata_pwm.current_motor1); // current motor 1
  ihm_CA[KIHM_CURVE_CURRENT].tval[1][ihm_val_idx] = (double) (pnd->navdata_pwm.current_motor2); // current motor 2
  ihm_CA[KIHM_CURVE_CURRENT].tval[2][ihm_val_idx] = (double) (pnd->navdata_pwm.current_motor3); // current motor 3
  ihm_CA[KIHM_CURVE_CURRENT].tval[3][ihm_val_idx] = (double) (pnd->navdata_pwm.current_motor4); // current motor 4

  ihm_CA[KIHM_CURVE_VZ].tval[3][ihm_val_idx] = (double) (pnd->navdata_pwm.vz_ref);  // VZ reference

  ihm_CA[KIHM_CURVE_VX].tval[0][ihm_val_idx] = (double) (pnd->navdata_vision_raw.vision_tx_raw);      // VISION trans. en x
  ihm_CA[KIHM_CURVE_VY].tval[0][ihm_val_idx] = (double) (pnd->navdata_vision_raw.vision_ty_raw);      // VISION trans. en y
  ihm_CA[KIHM_CURVE_VZ].tval[0][ihm_val_idx] = (double) (pnd->navdata_vision_raw.vision_tz_raw);      // VISION trans. en z


  if( pnd->vision_defined )
  {
    if( fabsf(pnd->navdata_vision_raw.vision_tx_raw) <= 10.0f && fabsf(pnd->navdata_vision_raw.vision_ty_raw) <= 10.0f )
    {
      ihm_dir = HOVER_VAL;
    }
    else
    {
      ihm_dir = (double) atan2f(pnd->navdata_vision_raw.vision_ty_raw, pnd->navdata_vision_raw.vision_tx_raw);
    }
  }
  else
  {
    ihm_dir = NOT_DEF_VAL;
  }

  //Vision States' display update for IHM
  vp_os_memset( label_vision_state_value, '\0', sizeof(label_vision_state_value) );
  sprintf(label_vision_state_value, "%08x", pnd->navdata_vision.vision_state);

  ihm_CA[KIHM_CURVE_VX].tval[1][ihm_val_idx] = (double) (pnd->navdata_demo.vx);      // Fusion Vx
  ihm_CA[KIHM_CURVE_VY].tval[1][ihm_val_idx] = (double) (pnd->navdata_demo.vy);      // Fusion Vy

#ifdef PC_USE_VISION
  draw_trackers_cfg.num_points = NUM_MAX_SCREEN_POINTS;
  vp_os_memset(&draw_trackers_cfg.locked[0], 0, NUM_MAX_SCREEN_POINTS * sizeof(uint32_t));
  vp_os_memcpy(&draw_trackers_cfg.locked[0], pnd->navdata_trackers_send.locked, NUM_MAX_SCREEN_POINTS * sizeof(uint32_t));
  vp_os_memset(&draw_trackers_cfg.points[0], 0, NUM_MAX_SCREEN_POINTS * sizeof(screen_point_t));
  vp_os_memcpy(&draw_trackers_cfg.points[0], pnd->navdata_trackers_send.point, NUM_MAX_SCREEN_POINTS * sizeof(screen_point_t));

  int i;
  draw_trackers_cfg.detected = pnd->navdata_vision_detect.nb_detected;
  for(i = 0 ; i < pnd->navdata_vision_detect.nb_detected ; i++)
  {
    draw_trackers_cfg.type[i]           = pnd->navdata_vision_detect.type[i];
    draw_trackers_cfg.patch_center[i].x = pnd->navdata_vision_detect.xc[i];
    draw_trackers_cfg.patch_center[i].y = pnd->navdata_vision_detect.yc[i];
    draw_trackers_cfg.width[i]          = pnd->navdata_vision_detect.width[i];
    draw_trackers_cfg.height[i]         = pnd->navdata_vision_detect.height[i];
  }
  set_draw_trackers_config(&draw_trackers_cfg);
#endif

  /*Stephane*/

	  extern char label_detection_state_value[32];
	  switch(pnd->navdata_demo.detection_camera_type)
	  {
		  case CAD_TYPE_NONE:  snprintf(label_detection_state_value,sizeof(label_detection_state_value),"Detection disabled"); break;
		  case CAD_TYPE_VISION:   snprintf(label_detection_state_value,sizeof(label_detection_state_value),"Searching 2D tags"); break;
		  case CAD_TYPE_COCARDE:  snprintf(label_detection_state_value,sizeof(label_detection_state_value),"Searching roundels"); break;
		  case CAD_TYPE_ORIENTED_COCARDE:  snprintf(label_detection_state_value,sizeof(label_detection_state_value),"Searching roundels"); break;
		  case CAD_TYPE_H_COCARDE:  snprintf(label_detection_state_value,sizeof(label_detection_state_value),"Searching H roundels"); break;
		  case CAD_TYPE_H_ORIENTED_COCARDE:  snprintf(label_detection_state_value,sizeof(label_detection_state_value),"Searching H roundels"); break;
		  case CAD_TYPE_STRIPE:  snprintf(label_detection_state_value,sizeof(label_detection_state_value),"Searching ground stripe (15Hz)"); break;
		  case CAD_TYPE_STRIPE_V:  snprintf(label_detection_state_value,sizeof(label_detection_state_value),"Searching ground stripe (60Hz)"); break;
		  default : snprintf(label_detection_state_value,sizeof(label_detection_state_value),"Navdata error");
	  }

	  char nbDetectedTags_label_buffer[1024];

	  if (pndvision->nb_detected==1 && ( pnd->navdata_demo.detection_camera_type==CAD_TYPE_ORIENTED_COCARDE ||  pnd->navdata_demo.detection_camera_type==CAD_TYPE_H_ORIENTED_COCARDE ) )
	  {  snprintf(nbDetectedTags_label_buffer,sizeof(nbDetectedTags_label_buffer),"Found : %i (%4.2f deg)",pndvision->nb_detected,pndvision->orientation_angle[0]); }
	  else if (pndvision->nb_detected==1 && (pnd->navdata_demo.detection_camera_type==CAD_TYPE_STRIPE || pnd->navdata_demo.detection_camera_type==CAD_TYPE_STRIPE_V))
	  {  snprintf(nbDetectedTags_label_buffer,sizeof(nbDetectedTags_label_buffer),"Found : %i (%4.2f deg - w: %i)",
			  pndvision->nb_detected,
			  pndvision->orientation_angle[0],
			  pndvision->width[0]);
	  }
	  else
	  {  snprintf(nbDetectedTags_label_buffer,sizeof(nbDetectedTags_label_buffer),"Found : %i",pndvision->nb_detected);	  }

	  if(nbDetectedTags_label!=NULL)
		  gtk_label_set_text((GtkLabel*)nbDetectedTags_label,(const gchar*)nbDetectedTags_label_buffer);





  gdk_threads_leave();

  return C_OK;
}