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Analysis of numerical integration techniques for real-time digital flight simulation / / by John W. Wilson and George G. Steinmetz
| Analysis of numerical integration techniques for real-time digital flight simulation / / by John W. Wilson and George G. Steinmetz |
| Autore | Wilson John W (John William), <1940-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , November 1968 |
| Descrizione fisica | 1 online resource (iii, 94 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Flight simulation
Flight simulators Numerical integration Numerical integration - Computer programs |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715931003321 |
Wilson John W (John William), <1940->
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| Washington, D.C. : , : National Aeronautics and Space Administration, , November 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Avionic pictorial tunnel-/pathway-/highway-in-the-sky workshops / / Russell V. Parrish, compiler
| Avionic pictorial tunnel-/pathway-/highway-in-the-sky workshops / / Russell V. Parrish, compiler |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2003 |
| Descrizione fisica | 1 online resource (v, 106 pages) : illustrations |
| Collana | NASA/CP |
| Soggetto topico |
Avionics
Display devices Flight control Enhanced vision Flight simulation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701387303321 |
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2003 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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CFD analysis of flexible thermal protection system shear configuration testing in the LCAT facility / / Paul G. Ferlemann
| CFD analysis of flexible thermal protection system shear configuration testing in the LCAT facility / / Paul G. Ferlemann |
| Autore | Ferlemann Paul G. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 |
| Descrizione fisica | 1 online resource (67 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Computational fluid dynamics
Thermal protection Test facilities Flight simulation Analysis (mathematics) Systems engineering |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Computational fluid dynamics analysis of flexible thermal protection system shear configuration testing in the Large Core Arc Tunnel facility |
| Record Nr. | UNINA-9910702673303321 |
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Ferlemann Paul G.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Check-cases for verification of 6-degree-of-freedom flight vehicle simulations / / Daniel G. Murri, E. Bruce Jackson, Robert O. Shelton
| Check-cases for verification of 6-degree-of-freedom flight vehicle simulations / / Daniel G. Murri, E. Bruce Jackson, Robert O. Shelton |
| Autore | Murri Daniel G. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January 2015 |
| Descrizione fisica | 1 online resource (2 volumes) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerospace vehicles
Commercial off-the-shelf products Degrees of freedom Flight simulation Three dimensional models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Check cases for verification of six degree of freedom flight vehicle simulations |
| Record Nr. | UNINA-9910703729803321 |
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Murri Daniel G.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A cockpit-display concept for executing a multiple glide-slope approach for wake-vortex avoidance / / Terence S. Abbott
| A cockpit-display concept for executing a multiple glide-slope approach for wake-vortex avoidance / / Terence S. Abbott |
| Autore | Abbott Terence S. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , February 1985 |
| Descrizione fisica | 1 online resource (41 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Cockpits
Air traffic control Flight simulation Display devices Vortex avoidance Aeronautical instruments - Display systems Glide path systems Wakes (Aerodynamics) Vortex-motion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709788303321 |
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Abbott Terence S.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , February 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Comparison of flight simulators based on human motion perception metrics / / Ana R. Valente Pais [and three others]
| Comparison of flight simulators based on human motion perception metrics / / Ana R. Valente Pais [and three others] |
| Autore | Valente Pais Ana R. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 2015 |
| Descrizione fisica | 1 online resource (49 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Motion perception
Flight simulation Visual stimuli Sensory perception Inertial guidance |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703786803321 |
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Valente Pais Ana R.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Concepts for conformal and body-axis attitude information for spatial awareness presented in a helmet-mounted display / / Denise R. Jones, Terence S. Abbott, and James R. Burley II
| Concepts for conformal and body-axis attitude information for spatial awareness presented in a helmet-mounted display / / Denise R. Jones, Terence S. Abbott, and James R. Burley II |
| Autore | Jones Denise R. |
| Pubbl/distr/stampa | Hampton, VA : , : NASA Langley Research Center, , March 1993 |
| Descrizione fisica | 1 online resource (8 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Attitude (inclination)
Flight simulation Helmet mounted displays Judgments Pilot performance |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707953003321 |
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Jones Denise R.
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| Hampton, VA : , : NASA Langley Research Center, , March 1993 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept / / H. Kevin Rivers
| Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept / / H. Kevin Rivers |
| Autore | Rivers H. Kevin |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1999 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
7 - Cyclic loads
Storage tanks Propellant tanks Load tests Load testing machines Flight simulation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Cyclic cryogenic thermal-mechanical testing of an X-33 reusable launch vehicle liquid oxygen tank concept |
| Record Nr. | UNINA-9910706133503321 |
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Rivers H. Kevin
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Dependence of dynamic modeling accuracy on sensor measurements, mass properties, and aircraft geometry / / Jared A. Grauer and Eugene A. Morelli
| Dependence of dynamic modeling accuracy on sensor measurements, mass properties, and aircraft geometry / / Jared A. Grauer and Eugene A. Morelli |
| Autore | Grauer Jared A. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2013 |
| Descrizione fisica | 1 online resource (40 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aircraft instruments
Aircraft stability Computer aided design Dynamic models Errors Flight simulation Mathematical models Measuring instruments Monte Carlo method |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702430103321 |
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Grauer Jared A.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight [[electronic resource] ] : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / / Anthony Neal Watkins ... [and others]
| Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight [[electronic resource] ] : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / / Anthony Neal Watkins ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (18 pages) : color illustrations |
| Altri autori (Persone) | WatkinsAnthony Neal |
| Collana | NASA/TM |
| Soggetto topico |
Pressure measurement
Pressure sensitive paints Flow distribution Flight simulation Pressure sensors Horizontal flight Blade tips |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight |
| Record Nr. | UNINA-9910701779103321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
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Flight simulation
(36)
- Display devices (6)
- Flight tests (5)
- Computerized simulation (4)
- Flight simulators (4)