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A Standard Kinematic Model for Flight Simulation at NASA AmesA standard kinematic model for aircraft simulation exists at NASA-Ames on a variety of computer systems, one of which is used to control the flight simulator for advanced aircraft (FSAA). The derivation of the kinematic model is given and various mathematical relationships are presented as a guide. These include descriptions of standardized simulation subsystems such as the atmospheric turbulence model and the generalized six-degrees-of-freedom trim routine, as well as an introduction to the emulative batch-processing system which enables this facility to optimize its real-time environment.
Document ID
19750006408
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Mcfarland, R. E.
(Computer Sciences Corp. Mountain View, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Publication Information
Publisher: NASA
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-CR-2497
Report Number: NASA-CR-2497
Accession Number
75N14480
Funding Number(s)
CONTRACT_GRANT: NAS2-7806
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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