Fourth mission : SCAO Engineer for Airbus Defense and Space (TESOA2)Objectives :Performing SCAO simulation to ensure all satellite requirements are coveredRealizations :Creation of reference test cases in order to model the behavior of the satellite (or some of its equipements) according to different operational scenariosValidation tests realized for ARROWHP (SADA behavior) and ARROW satellites (Custom Guidance laws for attitude control in Nominal mode)Production of Validation notesDebbuging of the simulator modelsNon regression tests and monitoring, Post processingConversion of Simulink models into reference and protected models (for Export Control purpose)Use of Matlab,Simulink and FAME simulator

Third mission : Flight control Engineer, as part of the Operation Division at CNESObjectives :- Keeping Earth Observation Satellites in operationRealizations :- Carrying out routine activities (platform experiments, station keeping maneuvers) and exceptional activities (avoidance maneuvers, flight software uploading, etc.) - Knowledge of each satellites’ platform equipments and payload- Treatment/analysis of anomalies and associate corrective procedures- Update/Creation of ground tools for post-processing and archiving (VBA coding)- Creating/Updating Flight Control Procedures, with validation tests on simulator- Training on numerous platforms: Proteus (CALIPSO, SMOS, JASON 3), ANGELS technology demonstrator, ISIS (training in progress)- Technical Qualification (QT) test activities in prevision of the MICROCARB satellite launch (MYRIADE platform)

Second mission : Design & Validation activities regarding the Flight Control Laws on the Single-Aisle NEO aircrafts (A319/A320/A321)Objectives : - Support to numerous NEO AutoPilot Lateral and Longitudinal Laws development activitiesRealizations :- Weight and CG estimator adjustment : Implementation and tests realized on simulator, using real flight tests data- Windshear warning system studies : Statistical study in order to validate the Windshear alarm and its compliance with the Airworthiness Authorities- Manual Flight control law validation, including non-regression testing- Lateral Law Innerloop study : Implementation of the new design within a simulator model, tests and post-treatment- Pitch Attitude Protection in Alternate Law - Tests and validation : Creation of flight points grid, generation and execution of scenarios in simulation- Preparation of an Autoland Certification file : Comparision between flight tests and simulations, writing of Simulation report for performance certification

First mission: Digitalization project in connexion with the Eurostar NEO Development (with Airbus Defense and Space) Sept. 24 2018 - March 29 2019Objectives: - Contributing to the industrialization and digitalization of the AOCS process for the Eurostar Neo product - Assisting in the development of a Database shared by all the fields of study (AOCS, mechanics, etc.)- Filling the Database and connecting it to AOCS analysis toolsRealizations:- Implementing links in the Database to ensure data uniqueness- Implementing data consistency tests to ensure their integrity (ex: Mass Centering Inertia), in Matlab and Java- Improving a dynamic generation tool, once connected to the Database- Connecting the CDR analysis process with the Database

Guidance - Attitude Engineer on the CNES Microcarb missionThe subject of the Master Thesis is part of the work on attitude guidance for the MicroCarb mission. The objective of this mission is to map the sources and sinks of CO2 on a global scale. The implementation of the instrument and the data processing are based on different acquisition and calibration modes that each require original and specific attitude guidance. This mission is also characterized by a very constrained development schedule with a launch planned for March 2021, which leads the DV / MP service (Programming Mission department of the Flight Dynamics service) to carry out studies of definition, feasibility, analysis and development of an operational guidance library.Objectives of the Master Thesis: defining and enriching the algorithms used to define the guidance laws and studying the induced performances in terms of data acquisition and respect of the constraints related to the satellite.

Participating in the MIST project was part of my Double Degree cursus, during my first year at KTH.The goal of this project is to design and construct a 3U Cubesat satellite with groups of KTH students, to be launched in the years to come.My participation consisted in a feasibility study of using a Raspberry Pi and its camera in the Cubesat.Link to the MIST blog: https://mistsatellite.space/

The Personal Initiative Project (PIP) was a group project that was part of my 2nd year at ISAE ENSICA. This project had to have a theme related to aeronautics or space.Our work was done as part of the 2015 Student Aerospace Challenge, and was therefore presented at the 8th Suborbital Day, on June 3, 2015.Project title: Predefinition of an augmented reality helmet with human-machine interfaceLink to the Student Aerospace Challenge website : http://www.studentaerospacechallenge.eu/index.php/en