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UAS Collision Avoidance Algorithm That Minimizes the Impact on Route Surveillance
A collision avoidance algorithm is developed and implemented that is applicable to different types
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Medical Devices, Supporting Networks, and Their Vulnerabilities
With the implementation of "one Air Force, one network" under way it is important to look at how th
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The Wind and Beyond
How ideas about aerodynamics first developed and how the science and technology evolved to forge th
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Flight Dynamic Response of HALE Aircraft to KC-135 Flowfield
This research effort examines the static affects of a KC-135 flowfield on a flexible winged Sensorc
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Technology Transfer
Everyday within United States Air Forces' research laboratories there are hundreds of scientists an
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Waste to Wealth
CRC Press 出版In an era of environmental challenges, Waste to Wealth: Emerging Technologies for Sustainable Devel
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High Altitude Airship Station-Keeping Analysis
Lighter-than-air vehicles were once widely utilized by most major militaries. The airship's extende
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Attitude Model of a Reaction Wheel/Fixed Thruster Based Satellite Using Telemetry Data
Attitude determination of satellites is normally the job of inertial instruments, such as gyroscope
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Reusable Launch Vehicle Design Implications for Regeneration Time
In last few years the Air Force Research Laboratory sponsored several research projects on Reusable
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Aerospace Ground Equipment Management's Impact on Homestation Sortie Production
Since the Air Force began its evolution into an Expeditionary Air Force, much effort has been expen
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Optimal Dynamic Soaring for Full Size Sailplanes
Dynamic soaring is a unique flying technique designed to allow air vehicles to extractenergy from h
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The Effect of Aerodynamic Surfaces Versus Thrust Maneuvers on Reentry Vehicles
This research effort analyzes the effect of aerodynamic surfaces versus thrust maneuvers on a reent
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Aircraft Maintenance Performance
The Air Force has implemented various aircraft maintenance organizational structures. The implement
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A Comparison of Nonlinear Algorithms to Prevent Pilot-Induced Oscillations Caused by Actuator Rate Limiting
Actuator rate limiting has contributed to Pilot-Induced Oscillations (PIO) on almost every new fly-
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Characterization Of Chlorinated Solvent Degradation in a Constructed Wetland
Widespread chlorinated ethene contamination of aquifers coupled with high costs of current treatmen
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Analysis and Forecasting of Air Force Operating and Support Cost for Rotary Aircraft
This research explores forecasting techniques to estimate the Cost per Flying Hour for Air Force He
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AMC's Hydrogen Future
The purpose of this research is to compare the costs associated with the transition to hydrogen air
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An Investigation of Starting Techniques for Inward Turning Inlets at Flight Speeds Below the On-Design Mach Number
The purpose of this study was to create and investigate starting techniques aimed at allowing compl
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Modeling a Field Application of In Situ Bioremediation of Perchlorate-Contaminated Groundwater Using Horizontal Flow Treatment Wells
Perchlorate contaminated groundwater is rapidly becoming a significant environmental remediation is
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Operational Characteristics of a Rotating Detonation Engine Using Hydrogen and Air
Rotating detonation engines (RDE) are pressure gain combustion engines that have the potential for
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Can You Create the Universal Pilot for the Universal Aircraft
Traditionally, fighter aircraft training has focused on exploiting the capabilities in the missions
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Development Document for Proposed Effluent Limitations Guidelines and Standards for Synthetic-Based Drilling Fluids and Other Non-Aqueous Drilling Fluids in the Oil and Gas Extraction Point Source Cat
The U.S. Environmental Protection Agency (EPA) was introduced on December 2, 1970 by President Rich
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Scaling Flight Tests of Unmanned Air Vehicles
Increasing technological advances and research interest in unmanned air vehicles(UAVs), have led to
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Integrating Automated Multi-Disciplinary Optimization in Preliminary Design of Non-Traditional Aircraft
Current methods of aircraft conceptual design lack the ability to quickly generate detailed analysi
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Experimental Methods to Characterize Nonlinear Vibration of Flapping Wing Micro Air Vehicles
For urban combat reconnaissance, the flapping wing micro air vehicle concept is ideal because of it
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Manufacturing and Evaluation of a Biologically Inspired Engineered MAV Wing Compared to the Manduca Sexta Wing Under Simulated Flapping Conditions
In recent years, researchers have expressed a vested interest in the concepts surrounding flapping
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Modeling Vertical Flow Treatment Wetland Hydraulics to Optimize Treatment Efficiency
An upward Vertical Flow Treatment Wetland (uVFTW) at Wright Patterson AFB designed to bioremediate
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A Comparative Analysis of Singe-State-to-Orbit Rocket and Air-Breathing Vehicles
This study compares and contrasts the performance of a variety of rocket and airbreathing, single-s
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Impact of Parameter Accuracy on Aircraft Structural Integrity Estimates
The USAF initiated the Aircraft Structural Integrity Program (ASIP) over 40 years ago because of ca
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An Evaluation of Formic Acid as an Electron Donor For Palladium Catalyzed Destruction of Nitroaromatic Compounds
The Department of Defense is responsible for over 2,000 hazardous waste sites containing nitroaroma
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Chromate Content Bias as a Function of Particle Size in Aircraft Primer Paint Overspray
Spray painting operations using chromate-containing primer paints produce particles which may expos
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Assembly, Integration, and Test Methods for Operationally Responsive Space Satellites
Current government and industry standards in spacecraft testing result in an Assembly, Integration,
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Analysis of Bacterial Population and Distribution in the Developing Strata of a Constructed Wetland Used for Chlorinated Ethene Bioremediation
Chlorinated hydrocarbons and their degradation products are among of the most common organic ground
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Computational Design of Upperstage Chamber, Aerospike, and Cooling Jacket for Dual-Expander Rocket Engine
To increase the performance of the current US satellite launch capability, new rocket designs must
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Optimized Dual Expander Aerospike Rocket
Research at the Air Force Institute of Technology (AFIT) focused on designing a cryogenic dual-expa
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Whole Spacecraft Vibration Isolation
The Department of Defense has identified launch vibration isolation as a major research interest. R
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A Comparative Analysis of the Cost Estimating Error Risk Associated With Flyaway Costs Versus Individual Components of Aircraft
A shrinking workforce, unstable budgets, and rapidly changing objectives under stricter time constr
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Critical Design Parameters for Pylon-Aided Gaseous Fuel Injection Upstream of a Flameholding Cavity
The Air Force Institute of Technology and the AFRL are investigating means to increase the efficien
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Development of a Screening Model for Design and Costing of an Innovative Tailored Granular Activated Carbon Technology to Treat Perchlorate-Contaminated Water
Perchlorate contamination of drinking water is a problem that has recently gained national attentio
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An Investigation Into Robust Wind Correction Algorithms for Off-the-Shelf Unmanned Aerial Vehicle Autopilots
This research effort focuses on developing methods to design efficient wind correction algorithms t
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Air Traffic Control Capabilities
New world-wide requirements to equip aircraft for ADS-B surveillance systems provides an opportunit
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Cycle Performance of a Pulse Detontation Engine With Supercritical Fuel Injection
Pulse detonation engines (PDE) rely on rapid ignition and formation of detonation waves. Because hy
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The Effects of Employing HVM on C-130 Aircraft at WR-ALC to Aircraft Availability
The objective of this research is to evaluate the impact of increasing the labor burn rate, one of
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Characterizing the Exhaust Plume of the Three-Electrode Micro Pulsed Plasma Thrusters
Three-electrode micro-PPTs are a new version of two electrode micro-PPTs devices. Performance predi
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Long Term Quadrotor Stabilization
The work of this thesis focuses on the IMU and getting the best performance possible out of the IMU
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