AIStorm.cxx

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// FGAIStorm - FGAIBase-derived class creates an AI thunderstorm or cloud
//
// Written by David Culp, started Feb 2004.
//
// Copyright (C) 2004  David P. Culp - davidculp2@comcast.net
//
// 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; either version 2 of the
// License, or (at your option) any later version.
//
// 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., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.
 
#include <cmath>
#include <cstdlib>
#include <string>
#include <time.h>
 
#include <Main/fg_props.hxx>
#include <Main/globals.hxx>
#include <Scenery/scenery.hxx>
 
#include "AIStorm.hxx"
 
 
FGAIStorm::FGAIStorm() : FGAIBase(object_type::otStorm, false)
{
   delay = 3.6;
   subflashes = 1;
   timer = 0.0;
   random_delay = 3.6;
   flash_node = fgGetNode("/environment/lightning/flash", true);
   flash_node->setBoolValue(false);
   flashed = 0; 
   flashing = false;
   subflash_index = -1;
   subflash_array[0] =  1;
   subflash_array[1] =  2;
   subflash_array[2] =  1;
   subflash_array[3] =  3;
   subflash_array[4] =  2;
   subflash_array[5] =  1;
   subflash_array[6] =  1;
   subflash_array[7] =  2;
 
   turb_mag_node = fgGetNode("/environment/turbulence/magnitude-norm", true);
   turb_rate_node = fgGetNode("/environment/turbulence/rate-hz", true);
}
 
 
void FGAIStorm::readFromScenario(SGPropertyNode* scFileNode) {
  if (!scFileNode)
    return;
 
  FGAIBase::readFromScenario(scFileNode);
 
  setDiameter(scFileNode->getDoubleValue("diameter-ft", 0.0)/6076.11549);
  setHeight(scFileNode->getDoubleValue("height-msl", 5000.0));
  setStrengthNorm(scFileNode->getDoubleValue("strength-norm", 1.0)); 
}
 
void FGAIStorm::update(double dt) {
   FGAIBase::update(dt);
   Run(dt);
   Transform();
}
 
 
void FGAIStorm::Run(double dt) {
   double speed_north_deg_sec;
   double speed_east_deg_sec;
 
   // convert speed to degrees per second
    speed_north_deg_sec = cos(hdg / SG_RADIANS_TO_DEGREES) * speed * 1.686 / ft_per_deg_lat;
    speed_east_deg_sec = sin(hdg / SG_RADIANS_TO_DEGREES) * speed * 1.686 / ft_per_deg_lon;
 
   // set new position
   pos.setLatitudeDeg( pos.getLatitudeDeg() + speed_north_deg_sec * dt);
   pos.setLongitudeDeg( pos.getLongitudeDeg() + speed_east_deg_sec * dt); 
 
   // do calculations for weather radar display 
   UpdateRadar(manager);
 
   // **************************************************
   // *     do lightning                               *
   // **************************************************
 
   if (timer > random_delay) {
     srand((unsigned)time(0));
     random_delay = delay + (rand()%3) - 1.0;
     //cout << "random_delay = " << random_delay << endl;
     timer = 0.0;
     flashing = true;
     subflash_index++;
     if (subflash_index == 8) subflash_index = 0; 
     subflashes = subflash_array[subflash_index]; 
   }
 
   if (flashing) {
     if (flashed < subflashes) {
         timer += dt;
         if (timer < 0.1) { 
         flash_node->setBoolValue(true);
         } else {
            flash_node->setBoolValue(false);
            if (timer > 0.2) {
              timer = 0.0;
              flashed++;
            }
         }
     } else {
       flashing = false;
       timer = 0.0;
       flashed = 0;
     }
    } else {
     timer += dt;
   }  
 
   // ***************************************************
   // *      do turbulence                              *
   // ***************************************************
 
   // copy user's position from the AIManager
   double d = dist(SGVec3d::fromGeod(pos), globals->get_aircraft_position_cart());
   double rangeNm =  d * SG_METER_TO_NM;
   double user_altitude = globals->get_aircraft_position().getElevationFt();
    
   if (rangeNm < (diameter * 0.5) &&
       user_altitude > (altitude_ft - 1000.0) &&
       user_altitude < height) {
              turb_mag_node->setDoubleValue(strength_norm);
              turb_rate_node->setDoubleValue(0.5);
   }
}