AirspeedAutocal constructor

AirspeedAutocal({ required float vx, required float vy, required float vz, required float diffPressure, required float eas2tas, required float ratio, required float stateX, required float stateY, required float stateZ, required float pax, required float pby, required float pcz, })

Implementation

AirspeedAutocal({
  required this.vx,
  required this.vy,
  required this.vz,
  required this.diffPressure,
  required this.eas2tas,
  required this.ratio,
  required this.stateX,
  required this.stateY,
  required this.stateZ,
  required this.pax,
  required this.pby,
  required this.pcz,
});