Aerodynamic Characteristics of Thin Cylindrical and Conical Shells in the Incompressible Flow
Closed-loop atmospheric ascent guidance based on finite element method
Computational Assessment of the Efficiency of Using Various Fuel Pairs Onboard a Small Spacecraft
Convex Approach to Three-Dimensional Launch Vehicle Ascent Trajectory Optimization
General Purpose Data-Driven Monitoring for Space Operations
New Algorithm for Probabilistic Robustness Analysis in Parameter Space
Simple Analytical Terminal Area Guidance for an Unpowered Reusable Launch Vehicle