发明名称 |
Compensated automatic gain control |
摘要 |
Circuitry for compensating for the effects of changes in ambient temperature on an automatic gain control arrangement in a missile-borne receiver is shown to include an operational amplifier responsive only to the level of the output signal from an automatic gain detector and amplifier, such end being effected by using temperature sensitive elements in the input and feedback circuits of the operational amplifier.
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申请公布号 |
US4185251(A) |
申请公布日期 |
1980.01.22 |
申请号 |
US19780912602 |
申请日期 |
1978.06.05 |
申请人 |
RAYTHEON |
发明人 |
BROWN, WILLIAM C JR;CRETE, PAUL G;SULLIVAN, PHILIP L;WILLIAMSON, JAMES |
分类号 |
G01S7/34;H03G3/20;(IPC1-7):H03G3/30 |
主分类号 |
G01S7/34 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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