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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/316 ; 244/321|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 10 인용 특허 : 0|
This invention relates to a servocontrol system for a weapon such as a missile which is a shoulder-launched, infrared-homing, guided missile which provides frontline troops with effective air defense against low altitude enemy aircraft. The weapon, described herein for purposes of illustration, consists of a missile and launcher combination which can be readily transported and operated within the normal environments associated with ground forces in a combat area. To meet the size, weight, and performance requirements, the missile achieves passive homing ...
A control system adapted to effect flight control of a rolling missile, said control system comprising a target seeker head mounted to the body of said missile and having means for generating electrical signals in accordance with the relative positions of the missile and an associated target, a plurality of fixed area lift producing variable incidence control surfaces extendable upon launch from within the missile body into the missile\s airstream and adapted to dither in the extended position for eliminating the inertial force caused by initial movement...