FULL-LENGTH PAPERS - Robust Autopilot for a Quasi-Linear Parameter-Varying Missile Model
Consensus-based reconfigurable controller design for unmanned aerial vehicle formation flight
Negative-g Trajectory Generation Using Quaternion-Based Inverse Dynamics
AIAA-2002-4659 Fuzzy Gain-Scheduling Flight Controller for a STT Missile
Pseudolinearing autopilot for a 6-DOF quasi-linear parameter varying missile model
Path Planning of UAVs in Urban Region Using Pythagorean Hodograph Curves
Dubins Path Planning of Multiple Unmanned Airborne Vehicles for Communication Relay
Robust Nonlinear Design of a High Incidence Missile Autopilot
Low Altitude Airborne SLAM with INS Aided Vision System AIAA Paper