|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/003.22 ; 244/003.1 ; 244/003.15 ; 244/003.21|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 6 인용 특허 : 30|
In a first aspect, the invention uses the thrust and axial aerodynamic forces of and on the missile system as the primary mechanism for altering the missile system's flight path as opposed to the missile system's aerodynamic normal force. In accordance with this first aspect, a first embodiment is a method for changing the direction of travel of a vehicle moving through a fluid medium to a desired direction of travel measured in the vehicle's inertial frame of reference, the vehicle comprising a body including a nose, a moment generating control device, ...
[ What is claimed:] [81.]81. A vehicle adapted for rapid redirection of the flight path and velocity as the vehicle is moving through a fluid medium at a velocity adequate for producing flight sustaining aerodynamic forces on the vehicle, said vehicle comprising:a body including a nose;a plurality of control devices, said control devices being-adapted to impart either a moment or a force to the vehicle in a manner such that the flight path and the velocity of the vehicle are rapidly redirected, said plurality of control devices comprising at least:a forw...