FULL-LENGTH PAPERS - Robust Autopilot for a Quasi-Linear Parameter-Varying Missile Model
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
Missile autopilot design using quasi-LPV polynomial eigenstructure assignment
Missile Autopilot Design using Quasi-LPV Polynomial Eigenstructure Assignment
Fuzzy logic consequent perturbation analysis for electric vehicles
Fuzzy logic consequent perturbation analysis for electric vehicles