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MAE3408 · Aerospace control

Official Handbook

2026 Handbook6 credit pointsLevel 3Department of Mechanical and Aerospace Engineering

Last checked: 23 Aug 2026 UTC

Overview

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.

#AssessmentTypeWeightHurdle
1AssignmentsWritten32%Threshold
2PracticalsWritten5%Threshold
3LaboratoryDemonstration3%Threshold
4Final assessmentExamination60%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

Joined by OR.

prohibitions

Joined by OR.

Learning outcomes

  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)

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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