Abstract: A method of aligning an aircraft with a landing platform in motion comprises measuring a GPS heading with at least one GPS sensor positioned at a known location relative to the landing platform while the landing platform is in motion, measuring an orientation of the aircraft with an orientation sensor fixed relative to the aircraft, calculating an orientation of the landing platform from the GPS heading, calculating an orientation offset between the measured orientation of the aircraft and the calculated orientation of the landing platform, and changing an orientation of the aircraft or the landing platform to reduce the orientation offset. A system for landing and securing an aircraft in an enclosure, a system for disconnecting a tether from an aircraft, and a system for landing an aircraft in an enclosure are also described.

Abstract: A fuel system damper for damping fuel pressure pulsations in a fuel rail includes a solid, flexible diaphragm which separates an upper chamber from a lower chamber. The upper chamber is sealed and contains a spring which is biased against the diaphragm. The lower chamber has an outlet to permit fuel to communicate with the diaphragm. The upper flange of the lower chamber extends inward at an angle to form a radial shoulder, and the diaphragm rests against and is supported by the shoulder. An attachment clip is fixedly attached between the upper and lower chambers and is positioned to securely engage the damper to a fuel injector cup.