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// FGAILocalTraffic - AIEntity derived class with enough logic to
// fly and interact with the traffic pattern.
//
// Written by David Luff, started March 2002.
//
// Copyright (C) 2002 David C. Luff - david.luff@nottingham.ac.uk
//
// 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.
# include <Main/globals.hxx>
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# include <Main/location.hxx>
# include <Scenery/scenery.hxx>
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# include <simgear/math/point3d.hxx>
# include <simgear/math/sg_geodesy.hxx>
# include <simgear/misc/sg_path.hxx>
# include <string>
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# include <math.h>
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SG_USING_STD ( string ) ;
# include "ATCmgr.hxx"
# include "AILocalTraffic.hxx"
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# include "ATCutils.hxx"
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FGAILocalTraffic : : FGAILocalTraffic ( ) {
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//Hardwire initialisation for now - a lot of this should be read in from config eventually
Vr = 70.0 ;
best_rate_of_climb_speed = 70.0 ;
//best_rate_of_climb;
//nominal_climb_speed;
//nominal_climb_rate;
//nominal_circuit_speed;
//min_circuit_speed;
//max_circuit_speed;
nominal_descent_rate = 500.0 ;
nominal_final_speed = 65.0 ;
//nominal_approach_speed;
//stall_speed_landing_config;
wind_from_hdg = 0.0 ;
wind_speed_knots = 0.0 ;
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}
FGAILocalTraffic : : ~ FGAILocalTraffic ( ) {
}
void FGAILocalTraffic : : Init ( ) {
// Hack alert - Hardwired path!!
string planepath = " Aircraft/c172/Models/c172-dpm.ac " ;
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SGPath path = globals - > get_fg_root ( ) ;
path . append ( planepath ) ;
aip . init ( planepath . c_str ( ) ) ;
aip . setVisible ( true ) ;
globals - > get_scenery ( ) - > get_scene_graph ( ) - > addKid ( aip . getSceneGraph ( ) ) ;
# define DCL_KEMT true
//#define DCL_KPAO true
# ifdef DCL_KEMT
// Hardwire to KEMT for now
// Hardwired points at each end of KEMT runway
Point3D P010 ( - 118.037483 , 34.081358 , 296 * SG_FEET_TO_METER ) ;
Point3D P190 ( - 118.032308 , 34.090456 , 299.395263 * SG_FEET_TO_METER ) ;
Point3D takeoff_end ;
bool d010 = true ; // use this to change the hardwired runway direction
if ( d010 ) {
rwy . threshold_pos = P010 ;
takeoff_end = P190 ;
rwy . hdg = 25.32 ; //from default.apt
patternDirection = - 1 ; // Left
pos . setelev ( rwy . threshold_pos . elev ( ) + ( - 8.5 * SG_FEET_TO_METER ) ) ; // This is a complete hack - the rendered runway takes the underlying scenery elev rather than the published runway elev so I should use height above terrain or something.
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} else {
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rwy . threshold_pos = P190 ;
takeoff_end = P010 ;
rwy . hdg = 205.32 ;
patternDirection = 1 ; // Right
pos . setelev ( rwy . threshold_pos . elev ( ) + ( - 0.0 * SG_FEET_TO_METER ) ) ; // This is a complete hack - the rendered runway takes the underlying scenery elev rather than the published runway elev so I should use height above terrain or something.
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}
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# else
//KPAO - might be a better choice since its in the default scenery
//Hardwire it to the default (no wind) direction
Point3D threshold_end ( - 122.1124358 , 37.45848783 , 6.8 * SG_FEET_TO_METER ) ; // These positions are from airnav.com and don't quite seem to correspond with the sim scenery
Point3D takeoff_end ( - 122.1176522 , 37.463752 , 6.7 * SG_FEET_TO_METER ) ;
rwy . threshold_pos = threshold_end ;
rwy . hdg = 315.0 ;
patternDirection = 1 ; // Right
pos . setelev ( rwy . threshold_pos . elev ( ) + ( - 0.0 * SG_FEET_TO_METER ) ) ; // This is a complete hack - the rendered runway takes the underlying scenery elev rather than the published runway elev so I should use height above terrain or something.
# endif
//rwy.threshold_pos.setlat(34.081358);
//rwy.threshold_pos.setlon(-118.037483);
//rwy.mag_hdg = 12.0;
//rwy.mag_var = 14.0;
//rwy.hdg = rwy.mag_hdg + rwy.mag_var;
//rwy.threshold_pos.setelev(296 * SG_FEET_TO_METER);
// Initial position on threshold for now
// TODO - check wind / default runway
pos . setlat ( rwy . threshold_pos . lat ( ) ) ;
pos . setlon ( rwy . threshold_pos . lon ( ) ) ;
hdg = rwy . hdg ;
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pitch = 0.0 ;
roll = 0.0 ;
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leg = TAKEOFF_ROLL ;
vel = 0.0 ;
slope = 0.0 ;
// Now set the position of the plane and then re-get the elevation!! (Didn't work - elev always returned as zero) :-(
//aip.setPosition(pos.lon(), pos.lat(), pos.elev() * SG_METER_TO_FEET);
//cout << "*********************** elev in FGAILocalTraffic = " << aip.getFGLocation()->get_cur_elev_m() << '\n';
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// Activate the tower - this is dependent on the ATC system being initialised before the AI system
AirportATC a ;
if ( globals - > get_ATC_mgr ( ) - > GetAirportATCDetails ( ( string ) " KEMT " , & a ) ) {
if ( a . tower_freq ) { // Has a tower
tower = ( FGTower * ) globals - > get_ATC_mgr ( ) - > GetATCPointer ( ( string ) " KEMT " , TOWER ) ; // Maybe need some error checking here
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freq = ( double ) tower - > get_freq ( ) / 100.0 ;
//cout << "***********************************AILocalTraffic freq = " << freq << '\n';
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} else {
// Check CTAF, unicom etc
}
} else {
cout < < " Unable to find airport details in FGAILocalTraffic::Init() \n " ;
}
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// Set the projection for the local area
ortho . Init ( rwy . threshold_pos , rwy . hdg ) ;
rwy . end1ortho = ortho . ConvertToLocal ( rwy . threshold_pos ) ; // should come out as zero
// Hardwire to KEMT for now
rwy . end2ortho = ortho . ConvertToLocal ( takeoff_end ) ;
//cout << "*********************************************************************************\n";
//cout << "*********************************************************************************\n";
//cout << "*********************************************************************************\n";
//cout << "end1ortho = " << rwy.end1ortho << '\n';
//cout << "end2ortho = " << rwy.end2ortho << '\n'; // end2ortho.x() should be zero or thereabouts
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Transform ( ) ;
}
// Run the internal calculations
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void FGAILocalTraffic : : Update ( double dt ) {
std : : cout < < " In FGAILocalTraffic::Update \n " ;
// Hardwire flying traffic pattern for now - eventually also needs to be able to taxi to and from runway and GA parking area.
FlyTrafficPattern ( dt ) ;
Transform ( ) ;
//cout << "elev in FGAILocalTraffic = " << aip.getFGLocation()->get_cur_elev_m() << '\n';
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// This should become if(the plane has moved) then Transform()
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}
// Fly a traffic pattern
// FIXME - far too much of the mechanics of turning, rolling, accellerating, descending etc is in here.
// Move it out to FGAIPlane and have FlyTrafficPattern just specify what to do, not the implementation.
void FGAILocalTraffic : : FlyTrafficPattern ( double dt ) {
// Need to differentiate between in-air (IAS governed) and on-ground (vel governed)
// Take-off is an interesting case - we are on the ground but takeoff speed is IAS governed.
bool inAir = true ; // FIXME - possibly make into a class variable
static bool transmitted = false ; // FIXME - this is a hack
// WIND
// Wind has two effects - a mechanical one in that IAS translates to a different vel, and the hdg != track,
// but also a piloting effect, in that the AI must be able to descend at a different rate in order to hit the threshold.
//cout << "dt = " << dt << '\n';
double dist = 0 ;
// ack - I can't remember how long a rate 1 turn is meant to take.
double turn_time = 60.0 ; // seconds - TODO - check this guess
double turn_circumference ;
double turn_radius ;
Point3D orthopos = ortho . ConvertToLocal ( pos ) ; // ortho position of the plane
//cout << "runway elev = " << rwy.threshold_pos.elev() << ' ' << rwy.threshold_pos.elev() * SG_METER_TO_FEET << '\n';
//cout << "elev = " << pos.elev() << ' ' << pos.elev() * SG_METER_TO_FEET << '\n';
switch ( leg ) {
case TAKEOFF_ROLL :
inAir = false ;
track = rwy . hdg ;
if ( vel < 80.0 ) {
double dveldt = 5.0 ;
vel + = dveldt * dt ;
}
IAS = vel + ( cos ( ( hdg - wind_from_hdg ) * DCL_DEGREES_TO_RADIANS ) * wind_speed_knots ) ;
if ( IAS > = 70 ) {
leg = CLIMBOUT ;
pitch = 10.0 ;
IAS = best_rate_of_climb_speed ;
slope = 7.0 ;
}
break ;
case CLIMBOUT :
track = rwy . hdg ;
if ( ( pos . elev ( ) - rwy . threshold_pos . elev ( ) ) * SG_METER_TO_FEET > 600 ) {
leg = TURN1 ;
}
break ;
case TURN1 :
track + = ( 360.0 / turn_time ) * dt * patternDirection ;
Bank ( 25.0 * patternDirection ) ;
if ( ( track < ( rwy . hdg - 89.0 ) ) | | ( track > ( rwy . hdg + 89.0 ) ) ) {
leg = CROSSWIND ;
}
break ;
case CROSSWIND :
LevelWings ( ) ;
track = rwy . hdg + ( 90.0 * patternDirection ) ;
if ( ( pos . elev ( ) - rwy . threshold_pos . elev ( ) ) * SG_METER_TO_FEET > 1000 ) {
slope = 0.0 ;
pitch = 0.0 ;
IAS = 80.0 ; // FIXME - use smooth transistion to new speed
}
// turn 1000m out for now
if ( fabs ( orthopos . x ( ) ) > 980 ) {
leg = TURN2 ;
}
break ;
case TURN2 :
track + = ( 360.0 / turn_time ) * dt * patternDirection ;
Bank ( 25.0 * patternDirection ) ;
// just in case we didn't make height on crosswind
if ( ( pos . elev ( ) - rwy . threshold_pos . elev ( ) ) * SG_METER_TO_FEET > 1000 ) {
slope = 0.0 ;
pitch = 0.0 ;
IAS = 80.0 ; // FIXME - use smooth transistion to new speed
}
if ( ( track < ( rwy . hdg - 179.0 ) ) | | ( track > ( rwy . hdg + 179.0 ) ) ) {
leg = DOWNWIND ;
transmitted = false ;
//roll = 0.0;
}
break ;
case DOWNWIND :
LevelWings ( ) ;
track = rwy . hdg - ( 180 * patternDirection ) ; //should tend to bring track back into the 0->360 range
// just in case we didn't make height on crosswind
if ( ( pos . elev ( ) - rwy . threshold_pos . elev ( ) ) * SG_METER_TO_FEET > 1000 ) {
slope = 0.0 ;
pitch = 0.0 ;
IAS = 90.0 ; // FIXME - use smooth transistion to new speed
}
if ( ( orthopos . y ( ) < 0 ) & & ( ! transmitted ) ) {
TransmitPatternPositionReport ( ) ;
transmitted = true ;
}
if ( orthopos . y ( ) < - 480 ) {
slope = - 4.0 ; // FIXME - calculate to descent at 500fpm and hit the threshold (taking wind into account as well!!)
pitch = - 3.0 ;
IAS = 85.0 ;
}
if ( orthopos . y ( ) < - 980 ) {
//roll = -20;
leg = TURN3 ;
transmitted = false ;
IAS = 80.0 ;
}
break ;
case TURN3 :
track + = ( 360.0 / turn_time ) * dt * patternDirection ;
Bank ( 25.0 * patternDirection ) ;
if ( fabs ( rwy . hdg - track ) < 91.0 ) {
leg = BASE ;
}
break ;
case BASE :
LevelWings ( ) ;
if ( ! transmitted ) {
TransmitPatternPositionReport ( ) ;
transmitted = true ;
}
track = rwy . hdg - ( 90 * patternDirection ) ;
slope = - 6.0 ; // FIXME - calculate to descent at 500fpm and hit the threshold
pitch = - 4.0 ;
IAS = 70.0 ; // FIXME - slowdown gradually
// Try and arrange to turn nicely onto base
turn_circumference = IAS * 0.514444 * turn_time ;
//Hmmm - this is an interesting one - ground vs airspeed in relation to turn radius
//We'll leave it as a hack with IAS for now but it needs revisiting.
turn_radius = turn_circumference / ( 2.0 * DCL_PI ) ;
if ( fabs ( orthopos . x ( ) ) < ( turn_radius + 50 ) ) {
leg = TURN4 ;
transmitted = false ;
//roll = -20;
}
break ;
case TURN4 :
track + = ( 360.0 / turn_time ) * dt * patternDirection ;
Bank ( 25.0 * patternDirection ) ;
if ( fabs ( track - rwy . hdg ) < 0.6 ) {
leg = FINAL ;
vel = nominal_final_speed ;
}
break ;
case FINAL :
LevelWings ( ) ;
if ( ! transmitted ) {
TransmitPatternPositionReport ( ) ;
transmitted = true ;
}
// Try and track the extended centreline
track = rwy . hdg - ( 0.2 * orthopos . x ( ) ) ;
//cout << "orthopos.x() = " << orthopos.x() << " hdg = " << hdg << '\n';
if ( pos . elev ( ) < = rwy . threshold_pos . elev ( ) ) {
pos . setelev ( rwy . threshold_pos . elev ( ) ) ; // + (-8.5 * SG_FEET_TO_METER)); // This is a complete hack - the rendered runway takes the underlying scenery elev rather than the published runway elev so I should use height above terrain or something.
slope = 0.0 ;
pitch = 0.0 ;
leg = LANDING_ROLL ;
}
break ;
case LANDING_ROLL :
inAir = false ;
track = rwy . hdg ;
double dveldt = - 5.0 ;
vel + = dveldt * dt ;
if ( vel < = 15.0 ) {
leg = TAKEOFF_ROLL ;
}
break ;
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}
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yaw = 0.0 ; //yaw = f(track, wind);
hdg = track + yaw ;
// Apply wind to ground-relative velocity if in the air
if ( inAir ) {
vel = IAS - ( cos ( ( hdg - wind_from_hdg ) * DCL_DEGREES_TO_RADIANS ) * wind_speed_knots ) ;
}
dist = vel * 0.514444 * dt ;
pos = dclUpdatePosition ( pos , track , slope , dist ) ;
}
void FGAILocalTraffic : : TransmitPatternPositionReport ( void ) {
// airport name + "traffic" + airplane callsign + pattern direction + pattern leg + rwy + ?
string trns = " " ;
trns + = tower - > get_name ( ) ;
trns + = " Traffic " ;
// FIXME - add the callsign to the class variables
trns + = " Trainer-two-five-charlie " ;
if ( patternDirection = = 1 ) {
trns + = " right " ;
} else {
trns + = " left " ;
}
// We could probably get rid of this whole switch statement and just pass a string containing the leg from the FlyPattern function.
switch ( leg ) { // We'll assume that transmissions in turns are intended for next leg - do pilots ever call out that they are in the turn?
case TURN1 :
// Fall through to CROSSWIND
case CROSSWIND : // I don't think this case will be used here but it can't hurt to leave it in
trns + = " crosswind " ;
break ;
case TURN2 :
// Fall through to DOWNWIND
case DOWNWIND :
trns + = " downwind " ;
break ;
case TURN3 :
// Fall through to BASE
case BASE :
trns + = " base " ;
break ;
case TURN4 :
// Fall through to FINAL
case FINAL : // maybe this should include long/short final if appropriate?
trns + = " final " ;
break ;
default : // Hopefully this won't be used
trns + = " pattern " ;
break ;
}
// FIXME - I've hardwired the runway call as well!! (We could work this out from rwy heading and mag deviation)
trns + = convertNumToSpokenString ( 1 ) ;
// And add the airport name again
trns + = tower - > get_name ( ) ;
Transmit ( trns ) ;
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}