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A study of a pilot's ability to control during simulated stability augmentation system failures [NASA TN D-1552]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. Nasa 1962Description: 36p.Subject(s): Augmentation

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NASA technical report

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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-1552 (Browse shelf)	Not for loan		TR15138

Total holds: 0

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Previous	NASA TN D-1470 Satellite motion in the vicinity of critical inclination	NASA TN D-1471 Tracking systems, their mathematical models and their errors [NASA TN D-1471]	NASA TN D-1521 An integral equation relating the general time-dependent lift and downwash distributions on finite wings in subsonic flow [NASA TN D-1521]	NASA TN D-1552 A study of a pilot's ability to control during simulated stability augmentation system failures [NASA TN D-1552]	NASA TN D-1553 Thermodynamic properties of carbon-dioxide and nitrogen mixtures behind a normal shock wave [ NASA TN D-1553 ]	NASA TN D-1554 Local pressure distribution on a blunt delta wing for angles of attack up to 35(degre) at mach numbers of 3.4 and 4.7 [ NASA TN D-1554 ]	NASA TN D-1555 Z-function solutions for the motion and heating during atmosphere entry from equatiorial orbits of a rotating planet [NASA TN D-1555]	Next

NASA technical report

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