Supports – With condition responsive control means
Patent
1980-03-13
1982-10-05
Schultz, William H.
Supports
With condition responsive control means
74 55, F16M 1300
Patent
active
043524818
ABSTRACT:
Gimbal ring 32 has torquer positioner 34 and position detector 36 connected by servo loop 38, 40. Vibration sensor 52 on ring 32 provides ring vibration signals to amplifier shifter 54, 58 and the resultant signals are added to the servo loop at amplifier 40 to damp out the detected vibration.
REFERENCES:
patent: 3606233 (1971-09-01), Scharton
patent: 3703999 (1972-11-01), Forys
patent: 3757093 (1973-09-01), Licata
patent: 4033541 (1977-07-01), Malveg
patent: 4179087 (1979-12-01), Johnson
patent: 4198025 (1980-04-01), Lowe
patent: 4270393 (1981-06-01), Osborne
Dicke, Jr. Allen A.
Hughes Aircraft Company
Karambelas A. W.
MacAllister W. H.
Schultz William H.
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