Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
Daniel Guggenheim School of Aerospace Engineering
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ItemOptimization for a mini-ramjet combustor for ace-power engines(Georgia Institute of Technology, 2009-07-14) Zinn, Ben T.
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ItemFault tolerant nonliner adaptive flight control for the X-33(Georgia Institute of Technology, 2009-07-14) Calise, Anthony J.
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ItemAgent-based simulations using human performance models for national airspace system risk assessment(Georgia Institute of Technology, 2009-07-14) Goldsman, David ; Alexopoulos, Christos ; Fujimoto, Richard M. ; Loper, Margaret L. ; Pritchett, Amy R.
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ItemGeorgia Tech contributions to the H&RT ultra lightweight, inflatable ...(Georgia Institute of Technology, 2009-07-14) Braun, Robert D.
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ItemCareer: artificial learning control systems for performance critical applications(Georgia Institute of Technology, 2009-04-30) Johnson, Eric N.
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ItemOptimal robust matching of engine models to test data(Georgia Institute of Technology, 2009-02-28) Mavris, Dimitri N. ; Denney, Russell
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ItemDesign and construction of an annular helicon closed drift thruster(Georgia Institute of Technology, 2009-01) Walker, Mitchell L. R. ; Kieckhafer, Alexander W.The Georgia Institute of Technology (GA Tech) has completed a three-phase process which developed an annular helicon plasma source and integrated it into a Hall Effect Thruster (HET). Phase 1 designed the annular helicon source and began plasma measurements using an RF-compensated Langmuir probe. Phase 2 extended the operating conditions of the annular helicon and used a highly-efficient commercial Langmuir probe unit for rapid data acquisition and development of design criteria for the Annular Helicon Closed Drift Thruster (AHCDT) device. Phase 3 took the results of Phase 2, developed the design for the AHCDT, and began performance testing. Initial tests of the AHCDT show that when operated at conditions similar to a HET, the thrust output of the AHCDT is within 10% of the original HET. Additionally, the AHCDT has shown the capability to operate at discharge voltages much lower than a HET, thus enabling future performance characterization and optimization at high thrust-to-power ratios.
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ItemAn energy-based thermodynamic stabilization framework for hybrid control design of large-scale aerospace systems(Georgia Institute of Technology, 2008-11-01) Haddad, Wassim M.
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ItemApproaches to TFM in the presence of uncertainty(Georgia Institute of Technology, 2008-09-30) Clarke, John-Paul B. ; Johnson, Ellis L. ; Singhose, William ; Solak, Senay ; Poage, JamesThe objective of this study was to support NASA milestone AS.1.4.05, which includes the development of probabilistic and stochastic methods for TFM to address uncertainties in weather predictions.
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ItemWavelets in control and optimization(Georgia Institute of Technology, 2008-09-16) Tsiotras, Panagiotis