Advances in Aerospace Guidance, Navigation and Control

Linear Parameter Varying Control of an Agile Missile Model Based on the Induced L2-norm Framework.- L2-norm Framework.- Improving the performance of an actuator control scheme during saturation.- Concurrent Learning Adaptive Model Predictive Control.- Model Reference Adaptive Control of Mildly Non-Linear Systems with Time Varying Input Delays - Part I Model Reference Adaptive Control of Mildly Non-Linear Systems with Time Varying Input Delays - Part II LFT model generation via 1-regularized least squares.- An Impulsive Input Approach to Short Time Convergent Control for Linear Systems.- Model Formulation of Pursuit Problem with Two Pursuers and One Evader.- Nonlinear Output-Feedback H Control for Spacecraft Attitude Control.