Organizational Unit:
Aerospace Systems Design Laboratory (ASDL)
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System Reliability Assessment using Covariate Theory
System-of-Systems Modeling for Personal Air Vehicles
Capturing Corporate Philosophy: The Future of IT
Technology for Rotorcraft Affordability Through Integrated Product/Process Development (IPPD)
Abstraction and Modeling Hypothesis for Future Transportation Architectures
Assessing the Impact of Mission Requirements, Vehicle Attributes, Technologies and Uncertainty in Rotorcraft System Design
Technology Infusion and Resource Allocation for a Civil Tiltrotor
An Integrated Decision-making Method to Identify Design Requirements Through Agent-based Simulation for Personal Air Vehicle System
Simultaneous Assessment of Requirements and Technologies in Rotorcraft Design
Implementation of a Technology Impact Forecast Technique on a Civil Tiltrotor