| 摘要 |
<p>The invention is a method for launching and recovering a child aircraft, manned or unmanned, as well as providing a method for continuous flight to and from a parent aircraft, manned or unmanned, from a pylon that is mounted externally or internally on the parent aircraft. The pylon mechanics are contained within the pylon, and controlled from the parent aircraft, through hard wiring or electronic signals via a data link, facilitated by antennas on both the parent aircraft and the pylon.</p> |
