|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||343/7ED ; 244/314 ; 343/5CM ; 343/16M|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 22 인용 특허 : 0|
An airborne missile guidance system is disclosed which consists of an airborne radar system with a monopulse antenna. The system receives returns from a radar-illuminated ground area including a target and in conjunction with a synthetic array data processor displays the illuminated area in terms of range and doppler frequency. Range and azimuth cursors are generated and displayed. These cursors represent controllable range and doppler frequency values. Manual means are provided to control the display so that when the target is displayed under the cursor...
A system for guiding a remotely controllable missile along a flight path towards a designated target area, said system comprising: radar means for transmitting energy to and receiving energy from a selected area of terrain, said radar means including a monopulse antenna having a pattern with a null plane in the azimuth dimension; cursor generator means, including manual control circuitry, for providing cursor signals indicative of the relative range and doppler frequency of a selected target portion in said terrain area as designated by the manual contro...