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flightgear/src/AIModel/AIBallistic.cxx

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3.2 KiB
C++

// FGAIBallistic - FGAIBase-derived class creates a ballistic object
//
// Written by David Culp, started November 2003.
// - 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., 675 Mass Ave, Cambridge, MA 02139, USA.
#ifdef HAVE_CONFIG_H
# include <config.h>
#endif
#include <simgear/math/point3d.hxx>
#include <math.h>
#include "AIBallistic.hxx"
FGAIBallistic::FGAIBallistic(FGAIManager* mgr) {
manager = mgr;
_type_str = "ballistic";
_otype = otBallistic;
}
FGAIBallistic::~FGAIBallistic() {
}
bool FGAIBallistic::init() {
FGAIBase::init();
vs = sin( elevation * 0.017453293 ) * speed;
hs = cos( elevation * 0.017453293 ) * speed;
aero_stabilized = true;
hdg = azimuth;
pitch = elevation;
return true;
}
void FGAIBallistic::bind() {
FGAIBase::bind();
}
void FGAIBallistic::unbind() {
FGAIBase::unbind();
}
void FGAIBallistic::update(double dt) {
FGAIBase::update(dt);
Run(dt);
Transform();
}
void FGAIBallistic::setAzimuth(double az) {
azimuth = az;
}
void FGAIBallistic::setElevation(double el) {
elevation = el;
}
void FGAIBallistic::setStabilization(bool val) {
aero_stabilized = val;
}
void FGAIBallistic::Run(double dt) {
double speed_north_deg_sec;
double speed_east_deg_sec;
double ft_per_deg_lon;
double ft_per_deg_lat;
// get size of a degree at this latitude
ft_per_deg_lat = 366468.96 - 3717.12 * cos(pos.lat()/SG_RADIANS_TO_DEGREES);
ft_per_deg_lon = 365228.16 * cos(pos.lat() / SG_RADIANS_TO_DEGREES);
// the two drag calculations below assume sea-level density,
// mass of 0.03 slugs, drag coeff of 0.295, frontal area of 0.007 ft2
// adjust horizontal speed due to drag
hs -= 0.000082 * hs * hs * dt;
if ( hs < 0.0 ) hs = 0.0;
// adjust vertical speed due to drag
if (vs > 0.0) {
vs -= 0.000082 * vs * vs * dt;
} else {
vs += 0.000082 * vs * vs * dt;
}
// convert horizontal speed (fps) to degrees per second
speed_north_deg_sec = cos(hdg / SG_RADIANS_TO_DEGREES) * hs / ft_per_deg_lat;
speed_east_deg_sec = sin(hdg / SG_RADIANS_TO_DEGREES) * hs / ft_per_deg_lon;
// set new position
pos.setlat( pos.lat() + speed_north_deg_sec * dt);
pos.setlon( pos.lon() + speed_east_deg_sec * dt);
// adjust vertical speed for acceleration of gravity
vs -= 32.17 * dt;
// adjust altitude (meters)
altitude += vs * dt * SG_FEET_TO_METER;
pos.setelev(altitude);
// adjust pitch if aerostabilized
if (aero_stabilized) pitch = atan2( vs, hs ) * SG_RADIANS_TO_DEGREES;
// set destruction flag if altitude less than sea level -1000
if (altitude < -1000.0) setDie(true);
}