FGInterface *f;
FGTime *t;
+
f = current_aircraft.fdm_state;
t = FGTime::cur_time_params;
// }
// get roll and pitch, convert to degrees
- int roll_deg = (int)(f->get_Phi() * RAD_TO_DEG);
- while ( roll_deg < -180 ) {
- roll_deg += 360;
+ double roll_deg = f->get_Phi() * RAD_TO_DEG;
+ while ( roll_deg <= -180.0 ) {
+ roll_deg += 360.0;
}
- while ( roll_deg > 179 ) {
- roll_deg -= 360;
+ while ( roll_deg > 180.0 ) {
+ roll_deg -= 360.0;
}
- int pitch_deg = (int)(f->get_Theta() * RAD_TO_DEG);
- while ( pitch_deg < -180 ) {
- pitch_deg += 360;
+ double pitch_deg = f->get_Theta() * RAD_TO_DEG;
+ while ( pitch_deg <= -180.0 ) {
+ pitch_deg += 360.0;
}
- while ( pitch_deg > 179 ) {
- pitch_deg -= 360;
+ while ( pitch_deg > 180.0 ) {
+ pitch_deg -= 360.0;
}
- int heave = (int)(f->get_W_body()) + 128;
+ short int heave = (int)(f->get_W_body() * 128.0);
// scale roll and pitch to output format (1 - 255)
// straight && level == (128, 128)
- int roll = (int)( (roll_deg+180.0) * 255.0 / 360.0) + 1;
- int pitch = (int)( (pitch_deg+180.0) * 255.0 / 360.0) + 1;
+ short int roll = (int)(roll_deg * 32768 / 180.0);
+ short int pitch = (int)(pitch_deg * 32768 / 180.0);
+
+ unsigned char roll_b1, roll_b2, pitch_b1, pitch_b2, heave_b1, heave_b2;
+ roll_b1 = roll >> 8;
+ roll_b2 = roll & 0x00ff;
+ pitch_b1 = pitch >> 8;
+ pitch_b2 = pitch & 0x00ff;
+ heave_b1 = heave >> 8;
+ heave_b2 = heave & 0x00ff;
+
+ sprintf( pve, "p%c%c%c%c%c%c\n",
+ roll_b1, roll_b2, pitch_b1, pitch_b2, heave_b1, heave_b2 );
- sprintf( pve, "p%c%c%c\n", roll, pitch, heave);
+ // printf( "p [ %u %u ] [ %u %u ] [ %u %u ]\n",
+ // roll_b1, roll_b2, pitch_b1, pitch_b2, heave_b1, heave_b2 );
FG_LOG( FG_SERIAL, FG_INFO, "roll=" << roll << " pitch=" << pitch <<
" heave=" << heave );