Units / MAE3408
MAE3408 · Aerospace control
2026 Handbook6 credit pointsLevel 3Department of Mechanical and Aerospace Engineering
Last checked: 23 Aug 2026 UTCOverview
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.
Offerings
The Handbook publishes no offerings for this unit.
Assessment
The Handbook lists an examination for this unit.
| # | Assessment | Type | Weight | Hurdle |
|---|---|---|---|---|
| 1 | Assignments | Written | 32% | Threshold |
| 2 | Practicals | Written | 5% | Threshold |
| 3 | Laboratory | Demonstration | 3% | Threshold |
| 4 | Final assessment | Examination | 60% | Threshold |
Continuous assessment: 40% Final assessment: 60% This unit contains hurdle requirements that you must achieve to be able to pass the unit. You are required to achieve at least 45% in the total continuous assessment component and at least 45% in the final assessment component. The consequence of not achieving a hurdle requirement is a fail grade (NH) and a maximum mark of 45 for the unit.
Assessment details may change. Please refer to the assessment information in Moodle closer to the start of the teaching period.
Requisites
prerequisite
- MAE2402 — Thermodynamics and gas dynamics
Learning outcomes
- Value the significance and relevance of systems and associated control in engineering
- 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
- Calculate the response of systems as a function of time using classical differential equation solution, Laplace transforms and state-space method
- 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
- Recognise the effects of non-linearity in systems and accept the limitations of the use of linear models as approximations
- Formulate solutions using computer-based techniques (such as Matlab)
Workload
The minimum total expected workload to achieve the learning outcomes for this unit is 144 hours per semester typically comprising a mixture of 3-6 hours of scheduled learning activities and 6-9 hours of independent study per week. Scheduled activities may include a combination of teacher-directed learning, peer-directed learning and online engagement. Independent study may include associated readings, assessment and preparation for scheduled activities.
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