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Simulink-Based Simulation Architecture for Evaluating Controls for Aerospace Vehicles (SAREC-ASV)The Simulation Architecture for Evaluating Controls for Aerospace Vehicles (SAREC-ASV) is a Simulink-based approach to providing an engineering quality desktop simulation capability for finding trim solutions, extracting linear models for vehicle analysis and control law development, and generating open-loop and closed-loop time history responses for control system evaluation. It represents a useful level of maturity rather than a finished product. The layout is hierarchical and supports concurrent component development and validation, with support from the Concurrent Versions System (CVS) software management tool. Real Time Workshop (RTW) is used to generate pre-compiled code for substantial component modules, and templates permit switching seamlessly between original Simulink and code compiled for various platforms. Two previous limitations are addressed. Turn around time for incorporating tabular model components was improved through auto-generation of required Simulink diagrams based on data received in XML format. The layout was modified to exploit a Simulink "compile once, evaluate multiple times" capability for zero elapsed time for use in trimming and linearizing. Trim is achieved through a Graphical User Interface (GUI) with a narrow, script definable interface to the vehicle model which facilitates incorporating new models.
Document ID
20060028176
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Christhilf, David m.
(Lockheed Martin Corp. Hampton, VA, United States)
Bacon, Barton J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2006
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA Paper 2006-6726
Report Number: AIAA Paper 2006-6726
Meeting Information
Meeting: AIAA Modeling and Simulation Technologies Conference and Exhibit
Location: Keystone, CO
Country: United States
Start Date: August 21, 2006
End Date: August 24, 2006
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 280-02-07
Distribution Limits
Public
Copyright
Public Use Permitted.
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