Abstract:Not Available Thin-film mirrors with inflatable support structures that incorporate piezoelectric materials for active control will be developed, evaluated, and integrated to provide increased precision in large deployable space systems. This structural shape control
Abstract:Not Available In this project, we will utilize the exponential dependence on voltage of the light output of a light emitting diode (LED). This characteristic will allow over 6 orders of magnitude change in intensity with better than 1% accuracy, when driven by the out
Abstract:Not Available The main motivation for a reconfigurable collision avoidance system is greater survivability, possible if the feedback system can reorganize itself in the presence of obstacles, actuator failures and surface damages. This project develops an autonomous in
Abstract:Not Available If the development of a vehicle capable of sustained hypersonic flight in the atmosphere at speeds above Mach 8 is to be realized, a ground-based wind tunnel with a reliable force measurement system is a necessity. However, above Mach 8, due to thermal s
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