Nonlinear Dynamic Inversion Flight Control Design for Guided Projectiles
Cooperative Docking Guidance and Control with Application to Civil Autonomous Aerial Refueling
Three-Dimensional Guidance Law for Target Enclosing Within Arbitrary Smooth Shapes
Incremental Passive Fault-Tolerant Control for Quadrotors Subjected to Complete Rotor Failures
Minimum-Fuel Closed-Loop Powered Descent Guidance with Stochastically Derived Throttle Margins
Distributed Optimization Method for Spacecraft Attitude Control and Vibration Suppression
Impact-Angle-Constrained Cooperative Guidance for Salvo Attack
Coordinated Orbit–Attitude–Vibration Control of a Sun-Facing Solar Power Satellite
Global Incremental Flight Control for Agile Maneuvering of a Tailsitter Flying Wing
Control and Guidance for Precision Deep Stall Landing
Switching Flight Control for Incremental Model-Based Dual Heuristic Dynamic Programming
Expanded Reference Models for Adaptive Control of Uncertain Systems with Actuator Dynamics
Output-Feedback Tube Model Predictive Control for Asteroid Circumnavigation and Descent
Sum-of-Squares Flight Control Synthesis for Deep-Stall Recovery
Stable Model Predictive Strategy for Rendezvous Hovering Phases Allowing for Control Saturation
Guidance Law Design with Fixed-Time Convergent Error Dynamics
Optimal Planar Powered Descent with Independent Thrust and Torque
Envelope Extension via Adaptive Augmented Thrust Vector Control System