Approach and Landing Range Guidance for an Unpowered Reusable Launch Vehicle
Designing Transfers to Geostationary Orbit Using Combined Chemical–Electric Propulsion
Efficient Computation of Optimal Interplanetary Trajectories Using Solar Electric Propulsion
Estimating Density Using Precision Satellite Orbits from Multiple Satellites
Estimating Density Using Precision Satellite Orbits from Multiple Satellites
Estimating Density Using Precision Satellite Orbits from Multiple Satellites
Path Clearance for Emergency Vehicles Through the Use of Vehicle-to-Vehicle Communication
Methodology for the Design of an Aerodynamic Package for a Formula SAE Vehicle
Active Flight Path Control for an Induced Spin Flight Termination System (AIAA 2018-0528)
State Variance-Based Approach to Flight Dynamic Constraints in Multidisciplinary Design Optimization
State Variance-Based Approach to Flight Dynamic Constraints in Multidisciplinary Design Optimization
A Neat Methanol Direct Injection Combustion System for Heavy-Duty Applications