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A system study for the application of microcomputers to research flight test techniquesThe onboard simulator is a three degree of freedom aircraft behavior simulator which provides parameters used by the interception procedure. These parameters can be used for verifying closed loop performance before flight. The air to air intercept mode is a software package integrated in the simulation process that generates a target motion and performs a tracking procedure that predicts the most likely next target position, for a defined time step. This procedure also updates relative position parameters and gives adequate fire commands. A microcomputer based on an aircraft spin warning system periodically samples the assymetric thrust and yaw rate of an airplane and then issues voice synthesized warnings and /or suggests to the ilot how to respond to the situation.
Document ID
19830011216
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smyth, R. K.
(University of Southern California Los Angeles, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Computer Operations And Hardware
Report/Patent Number
SR-8302-FTT-512
NASA-CR-169869
NAS 1.26:169869
Report Number: SR-8302-FTT-512
Report Number: NASA-CR-169869
Report Number: NAS 1.26:169869
Accession Number
83N19487
Funding Number(s)
CONTRACT_GRANT: NSG-4027
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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