diff = p.altitude_msl - last_alt;
if ( diff < -SGD_PI ) { diff += 2.0*SGD_PI; }
if ( diff > SGD_PI ) { diff -= 2.0*SGD_PI; }
- double theta = diff;
+ double theta = diff * 2.0;
if ( theta > 0.5*SGD_PI ) { theta = 0.5*SGD_PI; }
if ( theta < -0.5*SGD_PI ) { theta = -0.5*SGD_PI; }
theta_filter = 0.99*theta_filter + 0.01*theta;
fdm->left_flap = 0.0;
fdm->right_flap = 0.0;
+ fdm->elevator = -theta_filter * 5.0;
+ fdm->elevator_trim_tab = 0.0;
+ fdm->left_flap = 0.0;
+ fdm->right_flap = 0.0;
+ fdm->left_aileron = phi_filter * 1.5;
+ fdm->right_aileron = phi_filter * 1.5;
+ fdm->rudder = 0.0;
+ fdm->nose_wheel = 0.0;
+ fdm->speedbrake = 0.0;
+ fdm->spoilers = 0.0;
+
// Convert the net buffer to network format
fdm->version = htonl(fdm->version);
// cout << "p0 = " << p0.get_time() << " p1 = " << p1.get_time()
// << endl;
- double percent =
- (current_time - p0.get_time()) /
- (p1.get_time() - p0.get_time());
+ double percent;
+ if ( fabs(p1.get_time() - p0.get_time()) < 0.0001 ) {
+ percent = 0.0;
+ } else {
+ percent =
+ (current_time - p0.get_time()) /
+ (p1.get_time() - p0.get_time());
+ }
// cout << "Percent = " << percent << endl;
GPSPoint p = GPSInterpolate( p0, p1, percent );
+ // cout << current_time << " " << p0.lat_deg << ", " << p0.lon_deg << endl;
+ // cout << current_time << " " << p1.lat_deg << ", " << p1.lon_deg << endl;
cout << current_time << " " << p.lat_deg << ", " << p.lon_deg << endl;
send_data( p );