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Six-degree-of-freedom aircraft simulation with mixed-data structure using the applied dynamics simulation language, ADSIMA realistic simulation of an aircraft in the flight using the AD 100 digital computer is presented. The implementation of three model features is specifically discussed: (1) a large aerodynamic data base (130,00 function values) which is evaluated using function interpolation to obtain the aerodynamic coefficients; (2) an option to trim the aircraft in longitudinal flight; and (3) a flight control system which includes a digital controller. Since the model includes a digital controller the simulation implements not only continuous time equations but also discrete time equations, thus the model has a mixed-data structure.
Document ID
19900013751
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Savaglio, Clare
(Applied Dynamics International Ann Arbor, MI, United States)
Date Acquired
September 6, 2013
Publication Date
December 15, 1989
Publication Information
Publication: Jet Propulsion Lab., California Inst. of Tech., Proceedings of the 3rd Annual Conference on Aerospace Computational Control, Volume 2
Subject Category
Computer Programming And Software
Accession Number
90N23067
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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