The DoD high level architecture: an update
Proceedings of the 30th conference on Winter simulation
Distributed simulation of hybrid systems with AnyLogic and HLA
Future Generation Computer Systems - Parallel computing technologies (PaCT-2001)
Methods and tools for aerospace operations modeling and simulation: modeling the space shuttle
Proceedings of the 34th conference on Winter simulation: exploring new frontiers
A holistic usability framework for distributed simulation systems
A holistic usability framework for distributed simulation systems
HLA RTI performance evaluation
SIW '09 Proceedings of the 2009 SISO European Simulation Interoperability Workshop
Developing a web-enabled HLA federate based on portico RTI
Proceedings of the Winter Simulation Conference
RISE: A general simulation interoperability middleware container
Journal of Parallel and Distributed Computing
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This paper discusses an environment being developed to model a mission of the Space Launch System (SLS) and the Multipurpose Crew Vehicle (MPCV) being launched from Kennedy Space Center (KSC) to the International Space Station (ISS). Several models representing different phases of the mission such as the ground operations processes, engineered systems, and range components such as failure tree, blast, gas dispersion, and debris modeling are explained. These models are built using different simulation paradigms such as continuous, system dynamics, discrete-event, and agent-based simulation modeling. The High Level Architecture (HLA) is the backbone of this distributed simulation. The different design decisions and the information fusion scheme of this unique environment are explained in detail for decision-making. This can also help in the development of exploration missions beyond the International Space Station.