Spacecraft Orbital Mechanics

Learning Outcomes

Subject Specific Intellectual and Research Skills

Having successfully completed this module you will be able to:

•  apply and integrate knowledge and understanding of other engineering disciplines to support study of Orbital Mechanics and the ability to evaluate them critically and to apply them effectively (SM3m)
•  extract and evaluate pertinent data and to apply engineering analysis techniques in the solution of unfamiliar problems (EA6m)
•  identify, classify and describe the performance of systems and components through the use of analytical methods and modelling techniques (EA2m)
•  apply quantitative and computational methods, using alternative approaches and understanding their limitations, in order to solve space mission design and analysis problems and implement appropriate action (EA3m)
•  plan self-learning and improve performance, as the foundation for lifelong learning/CPD (G2m)
•  apply engineering techniques taking account of a range of commercial and industrial constraints (P10m)
•  monitor and adjust a personal programme of work on an on-going basis (G3m)
•  use fundamental knowledge to investigate new and emerging technologies (EA5)

Knowledge and Understanding

Having successfully completed this module, you will be able to demonstrate knowledge and understanding of:

•  know the characteristics of particular equipment, processes or products relevant to space mission design and analysis with extensive knowledge and understanding of a wide range of engineering materials and components (P2m)
•  know and understand design processes and methodologies in mission design and analysis, and apply and adapt them in unfamiliar situations (D10)
•  understand concepts relevant to Orbital Mechanics, some from outside engineering, and evaluate them critically and apply them effectively, including in engineering projects (SM6m, SM9m)
•  thoroughly understand current space mission design practice and its limitations, and some appreciation of likely new developments (P9m)
•  understand how Orbital Mechanics is applied in the context of mission development and spacecraft operations (P1m)
•  know and understand the mathematical and statistical methods necessary to underpin Orbital Mechanics, and to enable you to apply a range of mathematical methods, tools, and notations proficiently and critically in the analysis and solution of space mission design problems (SM2m)
•  show a comprehensive knowledge and understanding of mathematical and computational models relevant to Orbital Mechanics and an appreciation of their limitations (SM5m)
•  be aware of current problems and/or new insights most of which is at, or informed by, the forefront of mission design and analysis (SM8m)
•  demonstrate awareness that engineering activities should promote sustainable development and apply quantitative techniques where appropriate (EL11)
•  provide a comprehensive knowledge and understanding of scientific principles and methodology underpinning modern Orbital Mechanics to enable appreciation of the scientific and engineering context, and to support understanding of relevant historical, current and future developments and technologies (SM1m)
•  understand the relevant scientific principles of Orbital Mechanics (SM7m)
•  make general evaluations of risk issues in the context of mission design and analysis, including health & safety, environmental and commercial risk (EL13)
•  demonstrate awareness of developing technologies related to Orbital Mechanics (SM4m)

Revision of Mathematical Concepts

* Vector algebra

* Kinematics and Dynamics

* Planar and Spherical Trigonometry

Attitude Dynamics and Representation:

* Reference frames

* Euler’s equation

* Direction Cosine Matrix

* Euler Angles

* Quaternions

* Torque-free Motion

* Orbital Perturbations

Observations and Orbit Determination

* Observation Techniques

* Reference Frames and Time

* Preliminary Orbit Determination

Orbital Manoeuvres

* Coplanar Manoeuvres

* Non-Coplanar Transfers

Orbital Perturbations

* Non-Uniform Gravity Field

* Third-Body Perturbation

* Atmospheric Drag

* Solar Radiation Pressure

Orbital Propagation Techniques

* Analytical

* Semi-analytical

* Numerical

Relative Orbital Motion

* Relative Orbital Motion

* Linearisation & State Transition Matrix

Interplanetary Trajectories

* Lambert’s Problem

* Patched Conics

* Gravity-assisted fly-by trajectories

N-Body Problems

* N-Body Problem

* Circular Restricted Three-Body Problem

* Natural Dynamics around Libration Points

Teaching and learning methods

Teaching methods will include 36 lectures using a mix of slides and blackboard derivations. Panopto recordings of the lectures along with the slide deck will be made available on Blackboard wherever possible.

The lectures are complemented by 4 supervised 2h computer lab sessions as well as weekly office hours.

Further learning activities include directed reading and individual problem solving.

Resources & Reading list

General Resources

Matlab/Python and GMAT. Scientific computing environment and GMAT mission analysis tool (open source) will be used in the computer labs.

Summative

This is how we’ll formally assess what you have learned in this module.

Referral

This is how we’ll assess you if you don’t meet the criteria to pass this module.

Repeat

An internal repeat is where you take all of your modules again, including any you passed. An external repeat is where you only re-take the modules you failed.

Repeat Information

Repeat type: Internal & External