Component
École Nationale Supérieure d'Électrotechnique d'Électronique
Objectives
• Build the model, i.e. the set of differential equations governing the movement (attitude and position) of an aircraft in 3D space, taking into account the environment (gravity, aerology).
• Implement state space modelling and state feedback control for single-input and multi-input cases.
• Perform linear quadratic (LQ) state feedback synthesis and LQG control
• Understand standards for linear systems, H∞ requirements for closed-loop systems, H∞ control and H2 control for aeronautical vehicles
Description
This course examines the design of control laws for aeronautical vehicles.
Pre-requisites
• State space
• Non-linear control