Here's a patch to fix the asi problem (it affects most aircraft panels).
[ Avoids a sqrt( x < 0 ) ]
double p = _static_pressure_node->getDoubleValue();
double q = ( pt - p ) * INHGTOPSF; // dynamic pressure
- // Now, reverse the equation
+ // Now, reverse the equation (normalize dynamic pressure to
+ // avoid "nan" results from sqrt)
+ if ( q < 0 ) { q = 0.0; }
double v_fps = sqrt((2 * q) / SEA_LEVEL_DENSITY_SLUGFT3);
// Publish the indicated airspeed