Cifre - Phd Thesis - Dynamic Control Law For A Loads Protection Function (m/f)
Testia
Toulouse, France
Aerospace engineering masters degree
Automatic control theory
Aircraft loads and aeroelasticity
You will be part of a team developing all of our current and future commercial aircraft programmes, involved in research activities aiming at optimising the interface between systems and structure
Job Summary
You will be part of a team developing all of our current and future commercial aircraft programmes, involved in research activities aiming at optimising the interface between systems and structure.
The objective for this research PhD of 3 years is to develop an automatic loads protection function relying on a good observer of the loads plus recent automatic methodology.
Airbus offers attractive financial rewards, work-life balance initiatives, comprehensive wellbeing and health coverage, and great individual development opportunities.
Matching Summary
You will be part of a team developing all of our current and future commercial aircraft programmes, involved in research activities aiming at optimising the interface between systems and structure.
Skills & Requirements
Must-have
Aerospace Engineering Masters Degree
Automatic Control Theory
Aircraft Loads and Aeroelasticity
Matlab and Simulink proficiency
Python programming skills
Advanced English level
Nice-to-have
Multidisciplinary optimization support
Flexible working arrangements
Innovative thinking stimulation
Personal growth solutions
Key Requirements
Masters Degree in Aerospace Engineering or equivalent
Strong background in automatic control theory
Good knowledge of Aircraft Loads and Aeroelasticity