Attitude Model Predictive Control with Actuator Saturation Using an Arc-Search Interior-Point Method
Autonomous Spacecraft Attitude Reorientation Using Robust Sampled-Data Control Barrier Functions
Precise Control of Gimbal Systems with Model Reference Sliding Mode Controller
Adaptive Finite Time Intercept Guidance
Introduction to the F. Landis Markley Memorial Virtual Collection
Fault-Tolerant Reduced-Attitude Control for Spacecraft Constrained Boresight Reorientation
Gust Load Alleviation Using Reduced-Order Aeroelastic Models and Observer-Based Robust Control
Closed-Loop, Exact-Time, Minimum-Energy Attitude Control with Analytic Gain Selection
Robust Stability and Performance Analysis of Incremental Dynamic-Inversion-Based Flight Control Laws
New Solution to Euler’s Equations for Asymmetric Bodies: Applications to Spacecraft Reorientation
Facing Future Challenges in Feedback Control of Aerospace Systems Through Scientific Experimentation
Active Fault-Tolerant Incremental Sliding-Mode Flight Control Against Control Reversal
Reply by the Authors to G. Rapakoulias and P. Tsiotras
Low-Altitude Fixed-Wing Robust and Optimal Control Using a Barrier Penalty Function Method
Hierarchical Robust Model Prediction Control for a Long-Endurance Unmanned Aerial Vehicle
Passively Safe and Robust Multi-Agent Optimal Control with Application to Distributed Space Systems
Load Alleviation on Compound Rotorcraft Using Load Feedback and Extremum Seeking Control