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ON THE DESIGN OF A HIGH-GAIN SATURATING CONTROL SYSTEM FOR USE AS AN ADAPTIVE AUTOPILOT

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BookPublisher: Nasa, Washington, D.C. 1960Description: 48.DDC classification: NASA | TN D-305

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-305 (Browse shelf)	Not for loan		TR15950

Total holds: 0

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Previous	NASA TN D-303 THE HOT-PRESSING OF HAFNIUM CARBIDE (MELTING POINT, 7030 DEGREE F)	NASA TN D-304 AN EXPLORATORY INVESTIGATION OF SOME FACTORS INFLUENCING THE ROOM-TEMPERATURE DUCTILITY OF TUNGSTEN	NASA TN D-3041 NASA Technical Note : PERFORMANCE CORRELATION FOR ELECTRON-BOMBARDMENT ION SOURCES	NASA TN D-305 ON THE DESIGN OF A HIGH-GAIN SATURATING CONTROL SYSTEM FOR USE AS AN ADAPTIVE AUTOPILOT	NASA TN D-307 A HIGH-VELOCITY GUN EMPLOYING A SHOCK-COMPRESSED LIGHT GAS	NASA TN D-3071 Flight investigation of the aerodynamic properties of an ogee wing. [TN D 3071-TN D 3080]	NASA TN D-3072 Experimental profiles of velocity components and radial pressure distributions in a vortex contained in a short cylindrical chamber. [NASA TN D-3072]	Next

Bound With Nasa Tn D-301-04,306-10

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