Automated Design of Multiphase Space Missions Using Hybrid Optimal Control
High-Fidelity Aerostructural Optimization with a Geometrically Nonlinear Flutter Constraint
Numerical Optimization of Metasurface Cells for Acoustic Reflection
Optimal Robust Two-Body Trajectory Design with Corrective Maneuvers
Holistic Approach for Aircraft Trajectory Optimization Using Optimal Control
Jig-Shape Optimization of Low-Boom Supersonic Aircraft
Multidisciplinary Design Optimization of Transonic Wings with Boundary-Layer Suction
Aerodynamic Shape Optimization of Common Research Model Wing–Body–Tail Configuration
Optimal Low-Thrust Orbit Transfers Made Easy: A Direct Approach
Trajectory Planning for CubeSat Short-Time-Scale Proximity Operations
Aerodynamic Exergy-Based Analysis and Optimization of the Generic Hypersonic Vehicle Using FUN3D
Combining Shaping and Flow Control for Aerodynamic Optimization
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport
Particle Swarm Optimization Applied to Spacecraft Reentry Trajectory
Automatic Orbit Selection for a Radio Interferometric Spacecraft Constellation
Preliminary Design of Low-Energy, Low-Thrust Transfers to Halo Orbits Using Feedback Control
Surrogate Modeling Accelerated Shape Optimization of Deployable Composite Tape-Spring Hinges
Problem Formulations and Treatment of Uncertainties in Aerodynamic Design
Surface Mesh Movement Algorithm for Computer-Aided-Design-Based Aerodynamic Shape Optimization