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User's Guide for the Commercial Modular Aero-Propulsion System Simulation (C-MAPSS): Version 2This report is a Users Guide for version 2 of the NASA-developed Commercial Modular Aero-Propulsion System Simulation (C-MAPSS) software, which is a transient simulation of a large commercial turbofan engine (up to 90,000-lb thrust) with a realistic engine control system. The software supports easy access to health, control, and engine parameters through a graphical user interface (GUI). C-MAPSS v.2 has some enhancements over the original, including three actuators rather than one, the addition of actuator and sensor dynamics, and an improved controller, while retaining or improving on the convenience and user-friendliness of the original. C-MAPSS v.2 provides the user with a graphical turbofan engine simulation environment in which advanced algorithms can be implemented and tested. C-MAPSS can run user-specified transient simulations, and it can generate state-space linear models of the nonlinear engine model at an operating point. The code has a number of GUI screens that allow point-and-click operation, and have editable fields for user-specified input. The software includes an atmospheric model which allows simulation of engine operation at altitudes from sea level to 40,000 ft, Mach numbers from 0 to 0.90, and ambient temperatures from -60 to 103 F. The package also includes a power-management system that allows the engine to be operated over a wide range of thrust levels throughout the full range of flight conditions.
Document ID
20120003211
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Liu, Yuan
(N and R Engineering and Management Services Parma Heights, OH, United States)
Frederick, Dean K.
(Saratoga Control Systems Saratoga Springs, NY, United States)
DeCastro, Jonathan A.
(ASRC Aerospace Corp. Cleveland, OH, United States)
Litt, Jonathan S.
(NASA Glenn Research Center Cleveland, OH, United States)
Chan, William W.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
March 1, 2012
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-18125
NASA/TM-2012-217432
Report Number: E-18125
Report Number: NASA/TM-2012-217432
Funding Number(s)
WBS: WBS 457280.02.07.03.03.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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