|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||102/213 ; 102/213 ; 102/211 ; 102/214 ; 102/384 ; 244/003.15 ; 244/003.16 ; 244/003.19 ; 244/003.22 ; 342/062 ; 342/068|
|발명자 / 주소|
|인용정보||피인용 횟수 : 20 인용 특허 : 11|
A fuzing system for non-spinning or substantially non-spinning weapons is implemented by means of wide angle optics providing at least forward-hemisphere coverage, an array of infrared detectors and a microprocessor for image and data processing, aim-point selection, directional-warhead aiming and skewed-cone fuzing. The skewed-cone fuzing has a generatrix which is the vector sum of missile velocity, warhead velocity and the negative of target velocity.
[ Having thus described a preferred embodiment of the invention, it being understood that the disclosure is only illustrative and may not be deemed to limit the scope of protection hereof, what is claimed is:] [3.]3. In a substantially non-spinning guided missile, a passive-infrared-imaging fuze comprising at least one set of body-fixed wide-angle optics providing at least forward hemisphere coverage, a multi-element detector array and a microprocessor for image and data processing, aim-point selection and fuzing wherein said fuzing is skewed cone fuzing...