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COMPPENSATION BASED ON LINEARIZED ANALYSIS FOR A SIX-DEGREE-OF -FREEDOM MOTION SIMULATOR.

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BookPublisher: Nasa, Washington, D.C. 1973Description: 36.DDC classification: NASA | TN D-7349

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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-7349 (Browse shelf)	Not for loan		TR12075

Total holds: 0

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Previous	NASA TN D-7343 FORTRAN PROGRAM FOR CALCULATING VELOCITIES AND STREAMLINES ON THE HUB-SHROUD MID-CHANNEL FLOW SURFACE OF AN AXIAL OR MIXED-FLOW TURBOMACHINE.	NASA TN D-7345 COMPUTER PROGRAM FOR DEFINITION OF TRANSONIC AXILE-FLOW COMPRESSOR BLADE ROWS.	NASA TN D-7348 PROTON-RADIATION DAMAGE IN GUNN OSCILLLATORS.	NASA TN D-7349 COMPPENSATION BASED ON LINEARIZED ANALYSIS FOR A SIX-DEGREE-OF -FREEDOM MOTION SIMULATOR.	NASA TN D-7351 CORNERING CHARACTERISTICS OF A 40 X 14-16 TYPE VII AIRCRAFT TIRE AND A COMPARISON WITH CHARACTERISTICS OF A C40 X 14-21 CANTILEVER AIRCRAFT TIRE	NASA TN D-7352 BEAMR - AN INTERACTIVE GRAPHIC COMPUTER PROGRAM FOR DESIGN OF CHARGED-PARTICLE BEAM TRANSPORT SYSTEMS	NASA TN D-7353 CHARACTERISTICS AND PERFORMANCE OF A SUPERCONDUCTING BUMPY-TORUS MAGNETIC FACILITY FOR PLASMA RESEARCH	Next

Bound With Nasa Tn D-7340-48.Lack No-7342,44,46.

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