MAE3408 - Aerospace control - 2018

This unit commences with the modelling of various dynamic engineering systems, followed by the analysis of their transient and steady-state responses. More sophisticated analytical methods such as root locus and frequency response will be explored and will build the foundation for controller design in the future. Modelling via state-space methods will also be briefly covered.

At the end of this unit, students are expected to:

1. Value the significance and relevance of systems and associated control in engineering
2. Formulate linear dynamic mathematical models of various systems (mechanical, electrical, fluid, hydraulic and pneumatic) as well as graphical models (such as block diagrams and signal flow graphs) using time-domain, frequency-domain and state-space techniques together with the unified concept of resistance, capacitance and inertia/inductance
3. Calculate the response of systems as a function of time using classical differential equation solution, Laplace transforms and state-space method
4. Analyse the stability and dynamic performance of a system using root locus and Bode plot methods, and calculate system parameters to achieve the desired dynamic response
5. Recognise the effects of non-linearity in systems and accept the limitations of the use of linear models as approximations
6. Formulate solutions using computer-based techniques (such as Matlab)

Continuous assessment: 40%

Final Examination (3 hours): 60%

Students are required to achieve at least 45% in the total continuous assessment component and at least 45% in the final examination component and an overall mark of 50% to achieve a pass grade in the unit. Students failing to achieve this requirement will be given a maximum of 45% in the unit.

3 hours of lectures, 2 hours of tutorials and 6 hours of private study per week plus two 3-hour laboratories during semester.

See also Unit timetable information

Aerospace Engineering