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Antoine COUANON

Ramonville Saint Agne

Electionseuropéennes 2024

RETROUVEZ GRATUITEMENTLe résultat des européennes à Toulouse ainsi que le résultat des européennes en Haute-Garonne.

En résumé

Together with a technical-scientific graduate degree, I have some proven experience in the area of flight dynamics with the following social skills:

- Good relational and communication capabilities together with a team-player spirit
- Hard worker, Rigorous and Multitasks handler.
- Dynamic
- Adaptive and Quick learner
- Ability to adapt to a multicultural environment

Mes compétences :
Ingénierie
Aerospace

Entreprises

  • Collecte Localisation Satellites (cls) - Ingenieur d'exploitation

    Ramonville Saint Agne 2019 - maintenant

  • Telespazio - Aerospace engineer

    Rome 2018 - 2019 EGNOS System Evolutions & Correction

  • CS-SI for CNES - Aerospace engineer

    2014 - 2018 SAR/Galileo Operation Engineer

    Qualification of the future Search and rescue MEOLUT coordination ground control center (Cospas-sarsat)

  • CS-SI for CNES - Aerospace engineer

    2013 - 2014 Flight Dynamics IT technology department (SB/SP)

    Project: Development of the future Java-based CSO ground segment (MUSIS program).
    This was an Agile software development project (SCRUM) about building from scratch the flight dynamics algorithms of CSO user ground segment (using Orekit).
    The challenge was to design and develop the major functions of this Flight Dynamics Center in a timeframe of 1 year and a half.
    The development of this Flight Dynamics System ranged from the architectural design and development of the algorithms, the software specifications and the development of a lot of fight dynamics scientifics areas. The exigence of quality were very high and we have developed according to the ECSS standards. Moreover, we were in charge of the test strategy with the definition of test cases in accordance with the functional and performance requirements.

  • CS-SI - Aerospace engineer

    2013 - 2013 On my own initiative, I have developed a 2D / 3D visualisation tool based on OREKIT, a CS-owned low-level space dynamics Java-written library, through a collaborative work with the OREKIT developer’s team.
    I have worked in the development of propagators, perturbing forces, maneuvers planning and events detection for a flight dynamics software using OREKIT as low-level library.

  • CS-SI for CNES - Aerospace engineer

    2012 - 2013 Project: Software development (Java language) and feasibility study on the ships’ Automatic Identification System (AIS).
    The mission was to study the feasibility of a possible expansion of the current AIS from a local communication system (10km) to an international communication system based on a satellite constellation.
    This went through a Java-based development on a simulator to optimize the percentage of ships detection through different signal detection (deterministic or adaptive beam forming).

  • AUSY - Aerospace engineer

    Sèvres Cedex 2011 - 2012 Client : CNES (DCT/Radio Frequence/Hyperfréquences & Temps-Fréquence

    Project: Agile software development for software aiming to evaluate and monitor the performances (frequency and time stability) of a set of atomic clocks.
    Within a team of 3 engineers, I have contributed to the design of the software through a SCRUM Agile development. One of my tasks were the remote monitoring development, the algorithms and the clocks re-calibration monitoring using Java for the MMI and Scilab (Matlab) for the scientific part.
    This system contributes to the International atomic time.

  • CNES - Toulouse - Internship (6 mois)

    PARIS 1 2010 - 2010 Objective: The idea of PROBA-3 mission is to form a telescope through a satellites formation flying where the telescope mirror will be set on the target while the ocular will be on the chaser (Development in Scilab (Matlab)).
    My tasks on the PROBA-3 phase B mission analysis was to evaluate the performances of different scenarios between two satellites in formation flying:
    Evaluate all the orbital perturbations
    Spacecraft relative trajectory and relative velocity analysis
    Statistical analysis on different rendezvous scenarios as specified by ESA
    Fuel consumption analysis , accuracy and collision risk of different scenarios

  • Université Paul Sabatier Modélisation numérique de la trajectoire d’une sonde - Chargé d'étude (6 mois)

    2009 - 2010 Modélisation numérique de l’envoie d’une sonde de la Terre vers Saturne:


    • Étude du meilleur compromis rapidité/consommation afin d’atteindre l’objectif

    • Récupération des éphémérides et modélisation des orbites des corps célestes mis en jeu

    • Modélisation de l’assistance gravitationnelle (effet catapulte/swing-by) que subit la sonde lors de son passage proche d’une planète

    • Modélisation des trajectoires possibles et étude des performances

    • Programmation en langage C

  • Laboratoire d'électronique Université de Rouen - Stage (3mois)

    2008 - 2008 Etude théorique et expérimentale d'un banc de mesure hyperfréquence en bande X
    -Demande de devis et commande de matériels auprès du client
    -Travail en équipe
    -Rédaction d’un manuel d’utilisation

  • Modélisation de la houle Université Paul Sabatier - Chargé d'étude programmation

    2008 - 2009 -Etude Mathématique puis modélisation de la dynamique de la houle en fonction de la profondeur
    -Travail en équipe
    -Programmation en C

  • Acadomia - Cours à domicile

    Paris 2008 - 2009 Cours particuliers de Math/Physique/Chimie

Formations

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