Module overview
This module introduces advanced concepts of aerospace mechanics, dynamics and control.
The main focus is on dynamics, modeling and control of systems that have multiple degrees of freedom. The first part of the module aims to express the 3 translational and 3 rotational degrees of freedom of aircraft and spacecraft into a set of linearised ordinary differential techniques. The second part of the module analyses the linearised systems to identify the natural modes of motion for aerospace vehicles and their stability characteristics. The third part of the module introduces feedback control strategies that push aerospace vehicles towards desired performance criteria, e.g. reference tracking, improved stability, etc.
The lectures are complemented by computer-based laboratory sessions covering all relevant practical aspects on the analysis and design of closed-loop control systems.
Linked modules
University Computing Teaching Laboratories/ School of Engineering Labs & Computing Facilities are required. - Student access on own machines to a range of computational tools including Matlab, Simulink and Python is required. - [Demonstrators/ Module Tutors] 25:1 ratio of students: staff (demonstrators) for laboratory classes are required. - [Compute Equipment] Sufficient resource for in person learning sessions (Labs) for classes is required. External Repeat is allowed for students who have fulfilled the laboratory/workshop requirement of the module (set by Module Lead) in the original attempt.