15 Credits SPRING



Aims/Description: The module provides students with an understanding of the principles of aircraft flight dynamics and the problems of controlling aircraft¿s motion. It introduces the equations of motion for a rigid body aircraft and the aerodynamic forces and moments are then determined. Static and dynamic stability, response characteristics are defined and methods for their analysis are next introduced. Flying and handling qualities of an aircraft, and disturbances affecting its motion, are developed. The fundamentals of aircraft feedback control system design and analysis are introduced together with stability augmentation and automatic flight control systems. The module provides knowledge for state-space approaches for aircraft control and guidance systems linked with airworthiness requirements for flying qualities and stability.

Staff Contact: Prof L Mihaylova
Teaching Methods: Lectures, Tutorials, Laboratory work, Independent Study
Assessment: Formal Exam, Course work

Information on the department responsible for this unit (Automatic Control and Systems Engineering):

Departmental Home Page
Teaching timetable

|

NOTE
The content of our courses is reviewed annually to make sure it's up-to-date and relevant. Individual modules are occasionally updated or withdrawn. This is in response to discoveries through our world-leading research; funding changes; professional accreditation requirements; student or employer feedback; outcomes of reviews; and variations in staff or student numbers. In the event of any change we'll consult and inform students in good time and take reasonable steps to minimise disruption.

URLs used in these pages are subject to year-on-year change. For this reason we recommend that you do not bookmark these pages or set them as favourites.

Teaching methods and assessment displayed on this page are indicative for 2021-22. Students will be informed by the academic department of any changes made necessary by the ongoing pandemic.

Western Bank, Sheffield, S10 2TN, UK