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UTAH STATE UNIVERSITY
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You are viewing titles for UTAH STATE UNIVERSITY in the Aerospace engineering available through the UMI Dissertations & Thesis Gradwoorks site
Integration of ultrasonic consolidation and direct-write to fabricate a miniature synthetic aperture radar (SAR) phased array antenna
The history and dynamics of the plasma impedance probe
Development, simulation, and calibration of a flush air data system for a transatmospheric vehicle
The attitude determination and control system of the TOROID satellite
Uniform temperature infrared targets using ultrasonic consolidation
Aerodynamic and propulsion-assisted maneuvering for orbital transfer vehicles
Modeling, designing, fabricating, and testing of channel panel flat plate heat pipes
Thermal management strategy for the Hyperspectral Imager for the Coastal Ocean
Moving sphere simulations using the chimera grid approach
Active and attentive laser detection and ranging (LADAR) scanning for automatic target recognition
The adaptability of Langmuir probes to the pico-satellite regime
Terrain-relative and beacon-relative navigation for lunar powered descent and landing
A pipeline analog-to-digital converter for a plasma impedance probe
Embedded spacecraft thermal control using ultrasonic consolidation
Interim access to the International Space Station
Analysis of square-root Kalman filters for angles-only orbital navigation and the effects of sensor accuracy on state observability
Guidance and navigation linear covariance analysis for lunar powered descent
Architecture, inertial navigation, and payload designs for low-cost Unmanned Aerial Vehicle-based Personal Remote Sensing
Optimization of a low Reynold's number 2-D inflatable airfoil section
A linearly and circularly polarized active integrated antenna
Computational efficiency of a hybrid mass concentration and spherical harmonic modeling
Surface morphology implications on Langmuir probe measurements
Low-thrust assisted angles-only navigation
Experimental testing of the accuracy of attitude determination solutions for a spin-stabilized spacecraft
Investigation of the design and static behavior of cylindrical tubular composite adhesive joints utilizing the finite element method and stress-based failure theories
Distributed electrical power systems in Cubesat applications
Axisymmetric finite element modeling of adhesive joint between a laminated composite and metal cylinder
Aerodynamic thrust vectoring for attitude control of a vertically thrusting jet engine
Performance characterization of complex fuel port geometries for hybrid rocket fuel grains
Closed-loop thrust and pressure profile throttling of a nitrous oxide/hydroxyl-terminated polybutadiene hybrid rocket motor
Design and testing of digitally manufactured paraffin Acrylonitrile-butadiene-styrene hybrid rocket motors
Catalytic decomposition of nitrous oxide monopropellant for hybrid motor ignition
A formal approach to specifying and verifying spacecraft behavior
Angles-only navigation for autonomous orbital rendezvous
Development of modular thermal control architecture for modular satellites
Statistical methods for launch vehicle guidance, navigation, and control (GN&C) system design and analysis