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Servo loop design for air bearing inertial components [NASA TN D-1120]

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Material type: Text

TextLanguage: English Series: National Aeronautics and Space Administration (NASA)Publication details: Washington, D.C. NASA 1962Description: 16pSubject(s):

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		TR013941 [D-1120]

Total holds: 0

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Previous	Lunar storage of liquid propellants [NASA TN D-1117]	Gimbal geometry and attitude sensing of the ST-124 stablized platform [NASA TN D-1118]	Saturn vehicle attitude resolver computer error analysis [NASA TN D-1119]	Servo loop design for air bearing inertial components [NASA TN D-1120]	NASA Technical Note [NASA TN D-542]: Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor	NASA Technical Note [NASA TN D-543]: Fatigue-crack propagation in aluminum-alloy tension panels	NASA Technical Note [NASA TN D-544]: Measured base pressures on several twin rocket-nozzle configurations at mach numbers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins	Next

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