Pseudolinearing autopilot for a 6-DOF quasi-linear parameter varying missile model
FULL-LENGTH PAPERS - Robust Autopilot for a Quasi-Linear Parameter-Varying Missile Model
Robust Nonlinear Design of a High Incidence Missile Autopilot
AIAA-2002-4659 Fuzzy Gain-Scheduling Flight Controller for a STT Missile
Flight Control Design for a STT Missile: A Fuzzy LPV Approach