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Astronautik
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Electro-aerodynamic thrust for fixed-wing aircraft propulsion
Development, modeling and testing of a slow-burning solid rocket propulsion system
Modeling performance and noise of advanced operational procedures for current and future aircraft
Turbofan engine sizing and tradeoff analysis via signomial programming/
Feedback control of dynamical systems using neuromorphic vision sensors
Fuel benefit from optimal trajectory assignment on the North Atlantic tracks
Understanding the effect of cognitive reference frames on unmanned aircraft operations
Radiation dose to the global flying population
Reducing the air quality impacts of aircraft activity at airports
A model for sensitivity analysis of aircraft fleet evolution forecasting
Evaluation of propulsor aerodynamic performance for powered aircraft wind tunnel experiments
Predicting pilot intent and aircraft trajectory in uncontrolled airspace
The impact of aircraft design reference mission on fuel efficiency in the air transportation system
CubeSat attitude control using micronewton electrospray thruster actuation
Anomaly detection in airline routine operations using flight data recorder data
Aircraft cruise phase altitude optimization considering contrail avoidance