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{
10500 5200 679 450
0.865 0.36 0.01
0.004 1000.0
0.001 0.001 0.8
0.03 0.05 0.005
0.06 0.045 0.33
5.0 12.0
5.224 12.224 6.6
0.03 0.03 0.08
180 0.003 0.01 20
0.05 0.05
12.0
0.01 0.003
0.1 2.0
9.9 0.5
200
<0 0 0> 0.03
1 0
SABRE
}
#define PROP_TYPE 0
#define JET_TYPE 1
#define JET_AB_TYPE 2
#define TURBO_JET_TYPE 3
#define RADAR_TYPE_MASK 0x07L
#define PROP_TYPE 0
#define JET_TYPE 1
#define JET_AB_TYPE 2
#define TURBO_JET_TYPE 3
#define RADAR_TYPE_MASK 0x07L
class Flight_Specs
{
public:
float weight; /* weight in pounds */
float mass; /* mass in slugs (calculated, not in spec file) */
float max_thrust; /* maximum thrust in lbs/ft */
float max_speed; /* maximum speed in kts */
float corner_speed; /* optimal control speed */
float drag_factor; /* drag constant */
float idrag_factor; /* constant for induced drag */
float lift_factor; /* lift constant */
float wing_aoa; /* aoa of wing */
float max_aoa; /* beyond which, lift is 0 */
/* Factors increasing drag */
float drag_aoa, // drag produced by angle of attack
drag_yaw, // drag produced by yaw
drag_wb, // wheel brakes drag
drag_gr, // landing gear drag
drag_ab, // air brakes drag
drag_whls; // drag of wheels on ground
/* Rotational factors */
// Control factors
float control_pitch; // pitching moment produced by elevators/trim,
// proportional to elevator positon (-30...+30)
float control_yaw; // yawing moment produced by rudders
// proportional to rudder position (-30...+30)
float control_roll; // rolling moment produced by ailerons
// proportional to ailerons (-30...+30)
// Longitudinal & lattitidunal stability are
// effected by these
float return_pitch; // pitching moment produced to return to 0 angle of attack,
// proportional to angle of attack
float return_yaw; // yawing moment produced to return to 0 yaw
// proportional to yaw
// Rotational drag factors
float pitch_drag;
float yaw_drag;
float roll_drag;
// Damping limits
float pitch_damp;
float yaw_damp;
float roll_damp;
// landing limits
float lspeed; // maximum speed on ground
float l_z; // minimum vertical velocity
float l_aoa_max; // max aoa
float max_wb; // max vel for wheel brakes
// Adverse yaw & roll factors
float adv_yaw; // Adverse yaw produced by roll
float adv_roll; // Adverse roll produced by yaw
// More stuff!
float g_height; // height above ground, w/ gear down
float flap_lift; // how much flaps contrib to lift
float flap_drag; // and how much to drag
float damp_time; // how much time before applying damp ...
float wb_damp; // damping factor for wheel brakes
float g_limit; // limit on g's pulled
float stall_spin; // adverse spin produced by stalling
int max_damage; // Maximum amount of punishment
// And even more stuff!!
R_3DPoint view_point; // Where we look from when we're in
// the cockpit (in 'port' coords)
float max_aoa_factor; // for calc'ing max aoa as a function of vel
int engine_type; // 0 = prop, 1 = jet, 2 = jet with afterburner
long flags; // general-purpose flags
char model[9];
is >> fs.weight >> fs.max_thrust >> fs.max_speed >> fs.corner_speed;
is >> fs.lift_factor >> fs.max_aoa >> fs.wing_aoa;
is >> fs.drag_factor >> fs.idrag_factor ;
is >> fs.drag_aoa >> fs.drag_yaw >> fs.drag_wb;
is >> fs.drag_gr >> fs.drag_ab >> fs.drag_whls;
is >> fs.control_pitch >> fs.control_yaw >> fs.control_roll;
is >> fs.return_pitch >> fs.return_yaw;
is >> fs.pitch_drag >> fs.yaw_drag >> fs.roll_drag;
is >> fs.pitch_damp >> fs.yaw_damp >> fs.roll_damp;
is >> fs.lspeed >> fs.l_z >> fs.l_aoa_max >> fs.max_wb;
is >> fs.adv_yaw >> fs.adv_roll >> fs.g_height ;
is >> fs.flap_lift >> fs.flap_drag;
is >> fs.damp_time >> fs.wb_damp;
is >> fs.g_limit >> fs.stall_spin;
is >> fs.max_damage;
is >> fs.view_point >> fs.max_aoa_factor;
is >> fs.engine_type >> fs.flags;
is >> fs.model;
fs.model[8] = '\0';
#define PROP_TYPE 0
#define JET_TYPE 1
#define JET_AB_TYPE 2
#define TURBO_JET_TYPE 3
#define RADAR_TYPE_MASK 0x07L
class Flight_Specs
{
public:
float weight; /* weight in pounds */
float mass; /* mass in slugs (calculated, not in spec file) */
float max_thrust; /* maximum thrust in lbs/ft */
float max_speed; /* maximum speed in kts */
float corner_speed; /* optimal control speed */
float drag_factor; /* drag constant */
float idrag_factor; /* constant for induced drag */
float lift_factor; /* lift constant */
float wing_aoa; /* aoa of wing */
float max_aoa; /* beyond which, lift is 0 */
/* Factors increasing drag */
float drag_aoa, // drag produced by angle of attack
drag_yaw, // drag produced by yaw
drag_wb, // wheel brakes drag
drag_gr, // landing gear drag
drag_ab, // air brakes drag
drag_whls; // drag of wheels on ground
/* Rotational factors */
// Control factors
float control_pitch; // pitching moment produced by elevators/trim,
// proportional to elevator positon (-30...+30)
float control_yaw; // yawing moment produced by rudders
// proportional to rudder position (-30...+30)
float control_roll; // rolling moment produced by ailerons
// proportional to ailerons (-30...+30)
// Longitudinal & lattitidunal stability are
// effected by these
float return_pitch; // pitching moment produced to return to 0 angle of attack,
// proportional to angle of attack
float return_yaw; // yawing moment produced to return to 0 yaw
// proportional to yaw
// Rotational drag factors
float pitch_drag;
float yaw_drag;
float roll_drag;
// Damping limits
float pitch_damp;
float yaw_damp;
float roll_damp;
// landing limits
float lspeed; // maximum speed on ground
float l_z; // minimum vertical velocity
float l_aoa_max; // max aoa
float max_wb; // max vel for wheel brakes
// Adverse yaw & roll factors
float adv_yaw; // Adverse yaw produced by roll
float adv_roll; // Adverse roll produced by yaw
// More stuff!
float g_height; // height above ground, w/ gear down
float flap_lift; // how much flaps contrib to lift
float flap_drag; // and how much to drag
float damp_time; // how much time before applying damp ...
float wb_damp; // damping factor for wheel brakes
float g_limit; // limit on g's pulled
float stall_spin; // adverse spin produced by stalling
int max_damage; // Maximum amount of punishment
// And even more stuff!!
R_3DPoint view_point; // Where we look from when we're in
// the cockpit (in 'port' coords)
float max_aoa_factor; // for calc'ing max aoa as a function of vel
int engine_type; // 0 = prop, 1 = jet, 2 = jet with afterburner
long flags; // general-purpose flags
};
istream & operator >>(istream & is, Flight_Specs &fs)
{
char c = ' ';
while (is && c != '{')
is >> c;
if (!is)
return is;
is >> fs.weight >> fs.max_thrust >> fs.max_speed >> fs.corner_speed;
is >> fs.lift_factor >> fs.max_aoa >> fs.wing_aoa;
is >> fs.drag_factor >> fs.idrag_factor ;
is >> fs.drag_aoa >> fs.drag_yaw >> fs.drag_wb;
is >> fs.drag_gr >> fs.drag_ab >> fs.drag_whls;
is >> fs.control_pitch >> fs.control_yaw >> fs.control_roll;
is >> fs.return_pitch >> fs.return_yaw;
is >> fs.pitch_drag >> fs.yaw_drag >> fs.roll_drag;
is >> fs.pitch_damp >> fs.yaw_damp >> fs.roll_damp;
is >> fs.lspeed >> fs.l_z >> fs.l_aoa_max >> fs.max_wb;
is >> fs.adv_yaw >> fs.adv_roll >> fs.g_height ;
is >> fs.flap_lift >> fs.flap_drag;
is >> fs.damp_time >> fs.wb_damp;
is >> fs.g_limit >> fs.stall_spin;
is >> fs.max_damage;
is >> fs.view_point >> fs.max_aoa_factor;
is >> fs.engine_type >> fs.flags;
// m = W/g
fs.mass = fs.weight / g;
fs.max_speed = kts2fps(fs.max_speed);
fs.corner_speed = kts2fps(fs.corner_speed);
fs.lspeed = kts2fps(fs.lspeed);
fs.max_wb = kts2fps(fs.max_wb);
fs.g_height *= world_scale;
while (is && (c != '}'))
is >> c;
return is;
}
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