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B-737 Linear Autoland Simulink ModelThe Linear Autoland Simulink model was created to be a modular test environment for testing of control system components in commercial aircraft. The input variables, physical laws, and referenced frames used are summarized. The state space theory underlying the model is surveyed and the location of the control actuators described. The equations used to realize the Dryden gust model to simulate winds and gusts are derived. A description of the pseudo-random number generation method used in the wind gust model is included. The longitudinal autopilot, lateral autopilot, automatic throttle autopilot, engine model and automatic trim devices are considered as subsystems. The experience in converting the Airlabs FORTRAN aircraft control system simulation to a graphical simulation tool (Matlab/Simulink) is described.
Document ID
20040074342
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Belcastro, Celeste
(NASA Langley Research Center Hampton, VA, United States)
Hogge, Edward F.
(Lockheed Martin Corp. Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2004
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA/CR-2004-213021
Report Number: NASA/CR-2004-213021
Funding Number(s)
WORK_UNIT: WU 23-728-30-10
CONTRACT_GRANT: NAS1-00135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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