Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Design strategies for rotorcraft blades and HALE aircraft wings applied to damage tolerant wind turbine blade design
Prox-1 Guidance, Navigation, & Control Overview: Development, Algorithms, and Integrated Simulation
CONTRAST: A conceptual reliability growth approach for comparison of launch vehicle architectures
An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes
Testing the effects of violating component axioms in validation of complex aircraft systems
Architecting aircraft power distribution systems via redundancy allocation
A methodology for evaluating fleet implications of mission specification changes
Developing a computational model of the pilot's best possible expectation of aircraft state given vestibular and visual cues
Sustainability of multimodal intercity transportation using a hybrid system dynamics and agent-based modeling approach
Stochastic feasibility assessments of orbital propellant depot and commercial launch enabled space exploration architectures