|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||701/004 ; 244/003.21 ; 244/003.22|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 12 인용 특허 : 27|
A comparative dual-control strategy actuates forward and aft control devices simultaneously to significantly improve a missile's maneuverability/dynamic capability. A substantial, and measurable, operational effect of the inventive control strategy is a dramatic improvement in a missile's divert capability. To effect a maneuver in accordance with the inventive strategy, a missile's aft fins are initially deflected to generate a force OPPOSITE that conventionally used (pushing the missile's tail in the direction of the commanded maneuver) which simultaneo...
[ What is claimed is:] [15.]15. A method of maneuvering a vehicle, moving in a fluid medium, toward a direction of a commanded maneuver, said vehicle having:(i) a forward portion and a forward control device, and(ii) an aft portion and an aft control device, said method comprising:actuating said forward control device to generate a forward control force, acting on said forward portion, said forward control force having a component acting in a direction that is substantially the same as the direction of the commanded maneuver; andactuating said aft contro...