Publication Date:
2019-07-13
Description:
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.
Keywords:
Launch Vehicles and Launch Operations
Type:
AIAA Modeling and Simulation Technologies Conference; Aug 20, 2007 - Aug 23, 2007; Hilton Head, SC; United States
Format:
application/pdf
