NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Analog Simulation of Piloted Earth Reentry at Parabolic VelocityPiloted earth reentry at parabolic velocity was satisfactorily simulated by employing analog computing equipment. The ability of a pilot to control a spacecraft and to perform long- and short-range navigation tests was determined, In simulated emergency conditions the pilot accomplished a safe entry with a display presentation of only bank angle and longitudinal acceleration.
Document ID
19650036726
Acquisition Source
Langley Research Center
Document Type
Abstract
Authors
M T Moul (Langley Research Center Hampton, United States)
E J White (Langley Research Center Hampton, United States)
A A Schy (Langley Research Center Hampton, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Publication Information
Publication: Actes: Colloque International des Techniques de Calcul Analogique et Numerique en Aeronautique [Proceedings: International Symposium on Analogue and Digital Techniques Applied to Aeronautics]
Publisher: Presses Academiques Europeennes
Subject Category
Ground Support Systems and Facilities (Space)
Meeting Information
Meeting: Colloque International Des Techniques de Calcul Analogique Et Numerique en Aeronautique
Location: Liège
Country: BE
Start Date: September 9, 1963
End Date: September 12, 1963
Sponsors: Association Internationale pour le Calcul Analogique
Accession Number
65A19430
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Parabolic Velocity
Analog Simulation
Flight Simulation
Reentry Guidance
Pilot Performance

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19650036677Collected WorksActes: Colloque International des Techniques de Calcul Analogique et Numerique en Aeronautique [Proceedings: International Symposium on Analogue and Digital Techniques Applied to Aeronautics]
No Preview Available