z-logo
open-access-imgOpen Access
Simulation Environment for Orion Launch Abort System Control Design Studies
Author(s) -
John McMinn,
Edward Jackson,
David M. Christhilf
Publication year - 2007
Publication title -
aiaa modeling and simulation technologies conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2007-6881
Subject(s) - aerodynamics , abort , computer science , crew , control (management) , control system , software , systems engineering , software engineering , control engineering , simulation , engineering , operating system , aeronautics , aerospace engineering , electrical engineering , artificial intelligence
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. Nomenclature

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom