|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||364/424013 ; 244/321 ; 244/322|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 20 인용 특허 : 4|
A cooperative 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) while simultaneo...
A method for rapidly changing the direction of travel of a missile moving in a fluid medium to a desired new direction, said new direction being measured in the missile\s inertial frame of reference, said missile having (i) a forward portion and a forward thruster control device and (ii) an aft portion and an aft fin control device, said method comprising: (a) actuating (i) said forward thruster control device to generate a forward control force, acting on said forward portion, substantially in the desired new direction and (ii) said aft fin control devi...