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EFFECT OF REDUCED COMPUTER PRECISION ON A MIDCOURSE NAVIGATION AND GUIDANCE SYSTEM USING OPTIMAL FILTERING AND LINEAR PREDICTION

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BookPublisher: Nasa, Washington, D.C. 1966Description: 40.DDC classification: NASA | TN D-3382

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-3382 (Browse shelf)	Not for loan		TR13055

Total holds: 0

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Previous	NASA TN D-3309 TECHNIQUE FOR REMOVAL OF ANGULAR MOMENTUM FROM A SPACECRAFT MOMENTUM-EXCHANGE SYSTEM BY USE OF THE GRAVITY-GRADIENT MOMENTS	NASA TN D-3310 ANALYTICAL METHOD FOR DETERMINING FLOTATION STABILITY CHARACTERISTICS OF A RIGHT-CIRCULAR-CONIC FRUSTUM	NASA TN D-3363 COMPARATIVE MEASUREMENTS OF MAN'S WALKING AND RUNNING GAITS IN EARTH AND SIMULATED LUNAR GRAVITY	NASA TN D-3382 EFFECT OF REDUCED COMPUTER PRECISION ON A MIDCOURSE NAVIGATION AND GUIDANCE SYSTEM USING OPTIMAL FILTERING AND LINEAR PREDICTION	NASA TN D-3383 NUMERICAL SOLUTIONS FOR BLUNT AXISYMMETRIC BODIES IN A SUPERSONIC SPHERICAL SOURCE FLOW	NASA TN D-3384 A REVIEW OF FACTORS AFFECTING BOUNDARY-LAYER TRANSITION	NASA TN D-3385 AN INVESTIGATION OF SPLITTER PLATES FOR THE AERODYNAMIC SEPARATION OF TWIN INLETS AT MACH 2.5	Next

Bound With Nasa Tn D-3381,3383-90

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