FULL-LENGTH PAPERS - Robust Autopilot for a Quasi-Linear Parameter-Varying Missile Model
Consensus-based reconfigurable controller design for unmanned aerial vehicle formation flight
Nonlinear Model Predictive Coordinated Standoff Tracking of a Moving Ground Vehicle
Negative-g Trajectory Generation Using Quaternion-Based Inverse Dynamics
Robust Analysis for Missile Lateral Acceleration Control Using Finite Inclusion Theorem
Optimal Impact Angle Control Guidance Law Based on Linearization About Collision Triangle
Differential Geometric Guidance Based on the Involute of the Target's Trajectory