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
A Formal Approach for Decentralised Co-Ordination Among UAVs Using Hybrid Control
Differential Geometric Guidance Based on the Involute of the Target's Trajectory: 3-D Aspects
Multi-Objective Frequency Loop-Shaping of a Lateral Missile Autopilot
Robust Analysis for Missile Lateral Acceleration Control Using Finite Inclusion Theorem
Differential Geometric Guidance Based on the Involute of the Target's Trajectory
Fuzzy gain-scheduled missile autopilot design using evolutionary algorithms
Fuzzy Gain-Scheduled Missile-Autopilot Design using Evolutionary Algorithms