Roll Maneuverability of Transonic High-Aspect-Ratio-Wing Aircraft with Flared Folding Wingtips
Optimal Range Capabilities for Low-Lift-to-Drag Ratio Mars Entry Vehicles
Full-Envelope Flight Control for Compound Vertical Takeoff and Landing Aircraft
Fluid–Structure Coupled Analysis of Maneuver Load Alleviation on a Large Transport Aircraft
Rigid–Flexible Coupled Modeling and Flexoelectric Control for Flexible Rotating Structures
Numerical Study of Plasma Characteristics Under Magnetohydrodynamic Flow Control in Mars Entry
Attitude Hold Proportional Navigation Guidance for Interceptors with Off-Axis Seeker
Minimum-Drag Fault-Tolerant Aircraft Control Allocation via Online Lifting Line Calculation
Multi-User System for Earth Sensing Spacecraft Attitude Calibration and Analysis
Stable Optimal Feedback Control for Landers Based on Machine Learning
Piloted Simulation-Based Assessment of Simplified Vehicle Operations for Urban Air Mobility
Attitude Control of Flexible Multibody Spacecraft via Shape Change
Control Authority of a Single-Surface Parafoil with Bleed-Air Spoilers
General Dynamics for Single- and Dual-Axis Rotating Rigid Spacecraft Components
Enhanced Aerodynamic Performance of a Two-Dimensional Airfoil Using Moving Boundaries
Coupled Dynamics of Steady Jet Flow Control for Flexible Membrane Wings
Fluidic Flow Control Devices for Gust Load Alleviation
Improving Spacecraft Reliability Through Digital Transformation
Laminar Separation Control for Eppler 387 Airfoil Based on Resolvent Analysis
State Observing Method and Active Vibration Control Based on Virtual Sensing