发明名称 Aircraft, missile, projectile or underwater vehicle with improved control system and method of using
摘要 The present invention relates to an aircraft, missile, projectile or underwater vehicle with an improved control system, an improved control system and a method of maneuvering an aircraft, missile, projectile or underwater vehicle. More particularly, the present invention relates to an aircraft, missile, projectile or underwater vehicle with control surfaces that are movable along a track. The present invention further relates to a method of controlling a aircraft, missile, projectile or underwater vehicle using such a control system. One of the technical advantages of the control system on a track (or “tracked control surface”) over other aircraft, missile, projectile or underwater vehicle control systems is that the tracked control surface system enables the aircraft, missile, projectile or underwater vehicle to have an unlimited number of configurations, each configuration being tailored to the specific stability or maneuverability requirements during a specific portion of the flight.
申请公布号 US8809755(B1) 申请公布日期 2014.08.19
申请号 US200511292533 申请日期 2005.12.02
申请人 Orbital Research Inc. 发明人 Patel Mehul;Ng T. Terry;Suchy Paul
分类号 F42B10/12;B64C5/10 主分类号 F42B10/12
代理机构 代理人 Kolkowski Brian M.;Schmidt Robert Knecht
主权项 1. A method comprising: maneuvering an aircraft, missile, projectile or underwater vehicle by sensing a condition which requires a change in the center of pressure or a change in the static or dynamic stability of the aircraft, missile, projectile or underwater vehicle with at least one sensor having an output; and moving a control surface along a track positioned on the aircraft, missile, projectile or underwater vehicle's body wherein the moving of the control surface is performed by a control system based in part on the output of the at least one sensor.
地址 Cleveland OH US