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Aerospace dynamics. [ LMECA2830 ]


5.0 crédits ECTS  30.0 h + 30.0 h   1q 

Teacher(s) Chatelain Philippe ;
Language French
Place
of the course
Louvain-la-Neuve
Online resources

> https://icampus.uclouvain.be/claroline/course/index.php?cid=MECA2830

Prerequisites
  • Analytical mechanics
  • applied mathematics.
Main themes
  • Universal gravitation and applications.
  • Aircraft dynamics : equilibrium, stability and control.
  • Launchers.
  • Satellite orbits and attitude stability.
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:

  • AA1.1, AA1.2, AA1.3
  • AA2.1, AA2.2, AA2.3
  • AA3.1, AA3.3
  • AA5.1, AA5.2, AA5.4
  • AA6.1, AA6.2

Introduce students to the specific issues of aircraft dynamics, launcher systems and dynamics, and satellite dynamics.

Evaluation methods

Written exam in 2 parts:

  • theoretical questions
  • exercises
Content
  • Summary of rigid body mechanics.
  • Aircraft dynamics : aerodynamic loads, translational and rotational dynamics, steady state motion, propulsion, stability, controls.
  • Launcher dynamics and staging optimisation.
  • Satellite dynamics : orbits, transfers, rendezvous, attitude stability.
Bibliography
  • B. ETKIN Dynamics of Flight - Stability and Control.
  • L. GEORGE, J-F VERNET, J-C WANNER La mécanique du vol.
  • J.W. CORNELISSE, H.F.R. SCHÖYER, K.F. WAKKER Rocket Propulsion and Spaceflight.
Cycle et année
d'étude
> Master [120] in Electro-mechanical Engineering
> Master [120] in Mechanical Engineering
Faculty or entity
in charge
> MECA


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