|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 9 인용 특허 : 0|
An automatic frequency control system that is particularly suited for use with an aircraft launched radar controlled guided missile. The missile automatic frequency control system is made entirely of solid state devices including a voltage tuned solid state oscillator. The system employs a search mode of operation and two lock modes of operation. The search mode of operation occurs prior to missile launch when the aircraft radar and the missile control system are both scanning for a target and the reflected signal from the target has not been received by...
An automatic frequency control system comprising: a. first means for receiving reflected radar signals from a target; b. second means for receiving radar signals directly from a radar transmitter means; c. a voltage tuned solid state oscillator the output of which is connected tO said first and second means; d. third means responsive to the output of said second means for applying a first control voltage to said solid state oscillator; e. fourth means responsive to the output of said first means for applying a second control voltage to said solid state o...