Turbulence Model Effects on RANS Simulations of the HIFiRE Flight 2 Ground Test Configurations
TriTruss Packaging and Deployment Trade Study
Trajectory Optimization of Electric Aircraft Subject to Subsystem Thermal Constraints
Towards Characterizing the Variability in the Loading Demands of an Unmanned Aerial Vehicle
Toward Adaptation of fNIRS Instrumentation to Airborne Environments
Summary of the 1st AIAA Geometry and Mesh Generation Workshop (GMGW-1) and Future Plans
SUbsonic Single Aft eNgine (SUSAN) Power/Propulsion System Control Architecture Updates
Structured adaptive grid generation using algebraic methods
Statistical Approach on Utilizing Ground-based Experiments to Model Break-up Events
Spline Trajectory Algorithm Development: Bezier Curve Control Point Generation for UAVs
Spacecraft Mission Design for the Mitigation of the 2017 PDC Hypothetical Asteroid Threat
Rho-Isp Revisited and Basic Stage Mass Estimating for Launch Vehicle Conceptual Sizing Studies
Rho-Isp Revisited and Basic Stage Mass Estimating for Launch Vehicle Conceptual Sizing Studies
Quaternion normalization in additive EKF for spacecraft attitude determination
Profile-Following Entry Guidance Using Linear Quadratic Regulator Theory