1 // MagicCarpet.cxx -- interface to the "Magic Carpet" flight model
2 //
3 // Written by Curtis Olson, started October 1999.
4 //
5 // Copyright (C) 1999  Curtis L. Olson  - http://www.flightgear.org/~curt
6 //
7 // This program is free software; you can redistribute it and/or
8 // modify it under the terms of the GNU General Public License as
9 // published by the Free Software Foundation; either version 2 of the
10 // License, or (at your option) any later version.
11 //
12 // This program is distributed in the hope that it will be useful, but
13 // WITHOUT ANY WARRANTY; without even the implied warranty of
14 // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the GNU
15 // General Public License for more details.
16 //
17 // You should have received a copy of the GNU General Public License
18 // along with this program; if not, write to the Free Software
19 // Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.
20 //
21 // $Id$
22 
23 
24 #ifdef HAVE_CONFIG_H
25 #  include <config.h>
26 #endif
27 
28 #include <simgear/math/sg_geodesy.hxx>
29 
30 #include <Aircraft/controls.hxx>
31 #include <Main/globals.hxx>
32 #include <Main/fg_props.hxx>
33 
34 #include "MagicCarpet.hxx"
35 
36 
FGMagicCarpet(double dt)37 FGMagicCarpet::FGMagicCarpet( double dt ) {
38 //     set_delta_t( dt );
39 }
40 
41 
~FGMagicCarpet()42 FGMagicCarpet::~FGMagicCarpet() {
43 }
44 
45 
46 // Initialize the Magic Carpet flight model, dt is the time increment
47 // for each subsequent iteration through the EOM
init()48 void FGMagicCarpet::init() {
49     common_init();
50 }
51 
52 
53 // Run an iteration of the EOM (equations of motion)
update(double dt)54 void FGMagicCarpet::update( double dt ) {
55     // cout << "FGLaRCsim::update()" << endl;
56 
57     if (is_suspended())
58       return;
59 
60     // int multiloop = _calc_multiloop(dt);
61 
62     double time_step = dt;
63 
64     // speed and distance traveled
65     double speed = globals->get_controls()->get_throttle( 0 ) * 2000; // meters/sec
66     if ( globals->get_controls()->get_brake_left() > 0.0
67          || globals->get_controls()->get_brake_right() > 0.0 )
68     {
69         speed = -speed;
70     }
71 
72     double dist = speed * time_step;
73     double kts = speed * SG_METER_TO_NM * 3600.0;
74     _set_V_equiv_kts( kts );
75     _set_V_calibrated_kts( kts );
76     set_V_ground_speed_kt( kts );
77 
78     // angle of turn
79     double turn_rate = globals->get_controls()->get_aileron() * SGD_PI_4; // radians/sec
80     double turn = turn_rate * time_step;
81 
82     // update euler angles
83     _set_Euler_Angles( get_Phi(), get_Theta(),
84                        SGMiscd::normalizePeriodic(0, SGD_2PI, get_Psi() + turn) );
85     _set_Euler_Rates(0,0,0);
86 
87     // update (lon/lat) position
88     double lat2 = 0.0, lon2 = 0.0, az2 = 0.0;
89     if ( fabs( speed ) > SG_EPSILON ) {
90 	geo_direct_wgs_84 ( get_Altitude(),
91 			    get_Latitude() * SGD_RADIANS_TO_DEGREES,
92 			    get_Longitude() * SGD_RADIANS_TO_DEGREES,
93 			    get_Psi() * SGD_RADIANS_TO_DEGREES,
94 			    dist, &lat2, &lon2, &az2 );
95 
96         _set_Geodetic_Position( lat2 * SGD_DEGREES_TO_RADIANS,  lon2 * SGD_DEGREES_TO_RADIANS );
97     }
98 
99     // cout << "lon error = " << fabs(end.x()*SGD_RADIANS_TO_DEGREES - lon2)
100     //      << "  lat error = " << fabs(end.y()*SGD_RADIANS_TO_DEGREES - lat2)
101     //      << endl;
102 
103     double sl_radius, lat_geoc;
104     sgGeodToGeoc( get_Latitude(), get_Altitude(), &sl_radius, &lat_geoc );
105 
106     // update altitude
107     double real_climb_rate = -globals->get_controls()->get_elevator() * 5000; // feet/sec
108     _set_Climb_Rate( real_climb_rate / 500.0 );
109     double climb = real_climb_rate * time_step;
110 
111     _set_Geocentric_Position( lat_geoc, get_Longitude(),
112 			     sl_radius + get_Altitude() + climb );
113     // cout << "sea level radius (ft) = " << sl_radius << endl;
114     // cout << "(setto) sea level radius (ft) = " << get_Sea_level_radius() << endl;
115     _update_ground_elev_at_pos();
116     _set_Sea_level_radius( sl_radius * SG_METER_TO_FEET);
117     _set_Altitude( get_Altitude() + climb );
118     _set_Altitude_AGL( get_Altitude() - get_Runway_altitude() );
119 }
120 
121 
122 // Register the subsystem.
123 #if 0
124 SGSubsystemMgr::Registrant<FGMagicCarpet> registrantFGMagicCarpet;
125 #endif
126