The development and use of an interactive environment to perform control system design and analysis of the proposed Crew Exploration Vehicle Launch Abort System is described. The environment, built using a commercial dynamic systems design package, includes use of an open-source configuration control software tool and a collaborative wiki to coordinate between the simulation developers, control law developers and users. A method for switching between multiple candidate control laws and vehicle configurations is described. Aerodynamic models, especially in a development program, change rapidly, so a means for automating the implementation of new aerodynamic models is described.
Simulation Environment for Orion Launch Abort System Control Design Studies
AIAA Modeling and Simulation Technologies Conference ; 2007 ; Hilton Head, SC, United States
2007-08-20
Conference paper
No indication
English
Simulation Environment for Orion Launch Abort System Control Design Studies AIAA Paper
British Library Conference Proceedings | 2007
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