units
MAE5408
Faculty of Engineering
This unit entry is for students who completed this unit in 2015 only. For students planning to study the unit, please refer to the unit indexes in the the current edition of the Handbook. If you have any queries contact the managing faculty for your course or area of study.
Refer to the specific census and withdrawal dates for the semester(s) in which this unit is offered.
Level | Postgraduate |
Faculty | Faculty of Engineering |
Organisational Unit | Department of Mechanical and Aerospace Engineering |
Offered | Not offered in 2015 |
Coordinator(s) | M Thompson |
This unit gives an overview of the fundamental methods of orbital mechanics and spaceflight dynamics. It provides students with a coherent and unified framework for the mathematical modelling, analysis and control of space vehicles. The focus will be on the physical phenomena and analytical procedures required to understand and predict the behaviour of orbiting spacecraft. The students will see and appreciate how these methods are applied to real space systems and why spaceflight dynamics is a crucial tool in the development of any type of space mission.
The development and integration of students' knowledge in the theory of mechanics, electronics and physics based on previous study leading towards a mature understanding of current spaceflight dynamics technology within both a guided and self-learning environment.
Project work 20%
Assignments 30%
Examination (3 hours): 50%
3 hours lectures, 2 hours practical classes and 7 hours of private study per week
See also Unit timetable information