Flight Mechanics Test and Evaluation Adv (AERO5500)
UNIT OF STUDY
This unit aims to develop an understanding of aircraft flight test, validation and verification, and the development of modern flight control, guidance, and navigation systems. Students will gain skills in analysis, problem solving and systems design in the areas of aircraft dynamic system identification and control.
At the end of this unit students will be able to understand elements of the following: the principles of stability augmentation systems and autopilot control systems in aircraft operation, their functions and purposes; the characteristics of closed loop system responses; advanced feedback control systems and state-space design techniques; the concepts of parameter and state estimation; the design of observers in the state space and the implementation of a Kalman Filter; multi-loop control and guidance systems and the reasons for their structures; flight test principles and procedures and the implementation a flight test programme.
Further unit of study information
Lecture 3 hrs/week; Tutorial 2 hrs/week.
Through semester assessment (100%)
Faculty/department permission required?
Unit of study rules
Prerequisites and assumed knowledge
AERO5510 or AERO9560 or AERO3560, AERO5510 or AERO9560 or AERO3560, AERO5510 or AERO9560 or AERO3560
BE in the area of Aerospace Engineering or related Engineering field
Study this unit outside a degree
If you wish to undertake one or more units of study (subjects) for your own interest but not towards a degree, you may enrol in single units as a non-award student.
If you are from another Australian tertiary institution you may be permitted to underake cross-institutional study in one or more units of study at the University of Sydney.