A method for flying an aircraft includes flying the aircraft at a first
approximately level position and changing the flight of the aircraft from
the first approximately level position to a climbing position. The method
includes changing the flight of the aircraft from the climbing position to
a second approximately level position to achieve a weightless state during
the change to the second approximately level position and rolling the
aircraft during the weightless state using one or more rolling control
surfaces of the aircraft to establish a bank for a turn without creating
adverse yaw. The aircraft does not include a deflectable spoiler, fin or
rudder to counter adverse yaw. The rolling control surfaces of the
aircraft may comprise elevons of the aircraft.