Control System Design for a Ducted-Fan Unmanned Aerial Vehicle Using Linear Quadratic Tracker
Tracking control system based on linear quadratic (LQ) tracker is designed for a ducted-fan unmanned aerial vehicle (UAV) under full flight envelope including hover, transition, and cruise modes.To design the LQ tracker, a system matrix is augmented PROMOCODE with a tracking error term.Then the control input can be calculated to solve a single Ricc