Aerospace dynamics. [ LMECA2830 ]
5.0 crédits ECTS
30.0 h + 30.0 h
1q
Teacher(s) |
Chatelain Philippe ;
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Language |
French
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Place of the course |
Louvain-la-Neuve
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Online resources |
> https://icampus.uclouvain.be/claroline/course/index.php?cid=MECA2830
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Prerequisites |
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Analytical mechanics
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applied mathematics.
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Main themes |
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Universal gravitation and applications.
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Aircraft dynamics : equilibrium, stability and control.
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Launchers.
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Satellite orbits and attitude stability.
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Aims |
In consideration of the reference table AA of the program " Master's degree civil engineer mechanics ", this course contributes to the development, to the acquisition and to the evaluation of the following experiences of learning:
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AA1.1, AA1.2, AA1.3
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AA2.1, AA2.2, AA2.3
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AA3.1, AA3.3
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AA5.1, AA5.2, AA5.4
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AA6.1, AA6.2
Introduce students to the specific issues of aircraft dynamics, launcher systems and dynamics, and satellite dynamics.
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Evaluation methods |
Written exam in 2 parts:
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theoretical questions
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exercises
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Content |
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Summary of rigid body mechanics.
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Aircraft dynamics : aerodynamic loads, translational and rotational dynamics, steady state motion, propulsion, stability, controls.
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Launcher dynamics and staging optimisation.
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Satellite dynamics : orbits, transfers, rendezvous, attitude stability.
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Bibliography |
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B. ETKIN Dynamics of Flight - Stability and Control.
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L. GEORGE, J-F VERNET, J-C WANNER La mécanique du vol.
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J.W. CORNELISSE, H.F.R. SCHÖYER, K.F. WAKKER Rocket Propulsion and Spaceflight.
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Cycle et année d'étude |
> Master [120] in Mechanical Engineering
> Master [120] in Electro-mechanical Engineering
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Faculty or entity in charge |
> MECA
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