|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/315 ; 244/32 ; 244/321|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 27 인용 특허 : 0|
A guidance system for internally controlling the flight path of a missile includes a guidance platform having dispersion control means mounted on the guidance platform for detecting acceleration of the missile due to lift and side forces. The dispersion control means includes dispersion detection means to calculate the velocity and position errors relative to a drag-only trajectory from the detected acceleration due to the lift and side forces. The internal guidance system also includes missile positioning means for controlling the position of the missil...
A guidance system for controlling the flight path of a missile, the guidance system comprising: means for measuring lift and side forces due to external airflow, said measuring means comprising dispersion detection means for detecting acceleration of said missile due to the lift and side forces, said dispersion detection means further comprising means for calculating velocity error and position errors from the detected acceleration due to the lift and side forces; and means for compensating for the measured lift and side forces such that effects of the l...