N/A
PhD offer
Full-time
2100€ / month
Master's degree
Between 0 and 2 years
Doctoral student
01/03/2026
A PhD position is open in the Space Advanced Concepts Laboratory in collaboration with IMFT (institute de mécaniques des fluides des Toulouse)
Supervisors:
- Annafederica Urbano, professor, ISA-SUPAERO
- Sébastien Tanguy, professor, Université Paul Sabatier, IMFT
Technological context and scientific questions
During depressurization for propellant preconditioning (and cooling) prior to engine ignition or propellant transfer (in the context of space depots), bubbles can form and grow due to cavitation. This is a problem due to vapour accumulation under microgravity conditions and the impact on wall heat transfer. More generally, cavitation, under conditions where phase change predominates, is important for many applications (including nuclear power plants) and raises many questions that are not understood at the small scale.
This justifies the development of the SCREAMH2 microgravity wall cavitation experiment (currently in phase A/B development under an ESA contract), in which ISAE-SUPAERO is participating as part of the scientific team.
There are several scientific open questions regarding pool cavitation. It is unclear how the contact line phenomena (nano-region, wall roughness, cavity shape…), the level and dynamics of depressurization, and the nature of the fluid (pure or in the presence of non-condensable gas) impact the growth of these bubbles and the associated wall heat flux.
This thesis project aims to answer these questions by developing numerical models capable of accurately simulating pool cavitation, in parallel with the development of the SCREAMH2 experiment. The results will serve, on the one hand, as support for the experiment and, on the other hand, for its extension, particularly to configurations with multiple bubbles and in the presence of non-condensable gases.
Background
The present project is a continuation of the team’s recent work on the development of a solver for the direct numerical simulation of two-phase flows with phase change. The originality of the solver, based on a semi-implicit compressible projection method, lies in its thermodynamic consistency, which allows it to describe liquid, vapor, and saturation conditions at the interface for a generic fluid.
The solver has recently been extended to phase change in the presence of a contact line (solid, vapor, liquid) and validated for the simulation of nucleate boiling and pool cavitation. It has thus enabled parametric studies and model developments for bubble cavitation in microgravity at the wall. The models will be extended and generalized in this project.
This project aims to further develop the numerical solver and to use it to answer the scientific questions raised.
- Numerical development of the immersed boundary method [5] to include conjugate heat transfer and contact lines. After validation on basic test cases, configurations with complex geometries will need to be addressed. Initially, the simulation of CH4 pool cavitation used for validation in [4] will be reconsidered with the complex geometry (cylindrical support and cavity for the bubble).
- Incondensable gas. The solver will be extended to account for the presence of multi-species vapor and incondensable gases adsorption in the liquid while ensuring thermodynamic consistency at the interface. A surface tension model dependent on local composition will be developed, and the jump conditions will be adapted to take thermo-capillary effects into account. The model will need to be validated for simulation in the presence of Marangoni currents (using existing experimental data).
- Pool cavitation in micro-gravity. Several objectives will be pursued. The first will be to support the SCREAM H2 project with detailed numerical simulations. The second will be to extend the study of pool cavitation to many fluids, considering non-condensable gases and various geometric configurations. In particular, the phase change models developed in [4] will be extended and used to simulate multi-bubble configurations, the interaction between bubbles and their impact on wall heat transfer in microgravity.
Impact
While this project focuses on pool cavitation in microgravity, it is important to note that the developments envisaged are also intended to simulate and study other phenomena involving phase change in compressible flows in the presence of contact lines. These include 1) sloshing in tanks and 2) hydrodynamic cavitation with the development of cavitation pockets. It is planned to study such configurations towards the end of the thesis project, depending on how the project progresses.
Work environment
The PhD will be funded by CNES and will be hosted in the Space Advanced Concepts Laboratory at ISAE Supaero in collaboration with IMFT.
Towards mixed-initiative planning systems: building upon automated planning and plan recognition systems to construct solutions collaboratively
Additive manufacturing of functionnally graded materials
Post-doctoral offer
Full-time
3300€ / month
PhD
Post-doctoral research assistant
In the face of accidental events (collision, crash, impact of debris, etc.) or related to the context of the mission (military or terrorist aggression, etc.), the sensitive and functional zones of land, aeronautical and space vehicles, as well as ships and submarines, require protection systems that combine ballistic performance and lightness.
For a long time, the numerical optimisation of such protection systems came up against the problem of their manufacture. This limitation has been partly overcome thanks to the ongoing development of additive manufacturing techniques, which can now be used to produce functional materials with complex architecture. Often evaluated statically or under low-speed impact, there are still gaps in the performance of these materials under high-speed impact.
The aim of this project is to use metal additive manufacturing to develop materials with gradient properties and to assess their performance in ballistic energy absorption applications.
Lasbordes Air Operations Center (COAL)
The ISAE-SUPAERO flight operations center at Lasbordes airfield has a fleet of 8 light aircraft for teaching and research in the fields of flight mechanics and neuroergonomics.
The fleet is comprised of:
- 4 Aquila two-seater single-engine aircraft dedicated to initial flight instruction
- 3 single-engine, four-seater DR400s dedicated to initial flight instruction, training ISAE-SUPAERO students, and research activities
- 1 twin-engine Vulcanair P68 Observer 2, currently being instrumented for student training and research activities
This aircraft is equipped with a telemetry system, enabling a flight to be followed in real time from the institute’s classrooms. It also features sensors capable of recording the pilot’s eye activity (eye trackers), brain activity, and more. Versatile, with a large payload capacity, it can also be fitted with optical sensors via a hatch under the fuselage.
The COAL maintenance unit is responsible for the day-to-day operation of the aircraft, fleet maintenance, and regulatory monitoring of airworthiness.
It also prepares and examines aircraft modification files required for research and training flights.
COAL's Activities
- Pilot training on light aircraft, open to engineering cycle and master’s students.
- Practical work in flight mechanics and initiation to flight test techniques for students and continuing education.
- Research flights in the field of human factors and any other area requiring in-flight sensors.
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Design and Operation of Aerospace Vehicles Department (DCAS)
Our Research Department
The Department of Aerospace Vehicle Design and Control (DCAS) develops training and research activities to meet the scientific challenges of tomorrow’s air transportation and future space systems. It conducts cutting-edge research and develops advanced technologies, ranging from human-machine interactions to the integrated multidisciplinary design of aircraft or advanced space concepts, via system control and control laws.
Our research incorporates environmental and socio-economic aspects, such as reducing environmental impacts (fuel consumption, noise, emissions), optimising design cycle times and operational costs, increasing the safety of aerospace systems, and improving the efficiency of man-machine systems.
Permanent staff
Doctoral students, post-doctoral students and engineers
Aircraft
Sponsorship chairs
At DCAS, we design the aerospace systems of the future, integrating performance, sustainability and safety. Our research combines advanced technologies, systems intelligence and environmental responsibility to reinvent air and space transport.
Valérie Budinger Head of DepartmentOur Research Activities
DCAS is structured into 4 scientific groups:
- Decision and Control (DC): Dynamic and operational behaviour models, synthesis of control laws and sequential decision algorithms.
- Aeronautical Vehicle Design and Flight Dynamics (CADV ): Aircraft design, flight dynamics, aircraft operation and certification, sustainable air transportation
- Space Systems Design (CSS): Orbital systems, mission analysis, space systems design and optimisation, space exploration and access to space
- Humans, Systems and Interactions (HSI ): Monitoring and optimisation of human performance in contexts of interaction with natural or technological environments
They work collaboratively on the following 3 interdisciplinary themes:
The aims of this theme are to carry out research into the identification and control of degraded flight situations:
- Aircraft/drone: Critical flight situations (e.g. departure from flight envelope, inconsistency of complex parameters/pannes, sub-system failures)
- Crew/operator: Borderline cognitive states (e.g. attentional tunnelling, perseveration, fatigue)
- Guaranteeing control performance that is independent of uncertainties and parametric variations
- Defining 'intelligent' control and supervision processes to optimise flight safety
- Developing an adaptive control and driving system that is robust to failures
With the help of the many resources made available by the department - DCAS simulators, flying platforms (TB20, etc.), Neuroergo-lab, indoor aviary - this theme enables DCAS to innovate in the field of human factors (with the development of adaptive cockpits) and automation/decision: Fail-safe laws, self-reconfigurable control system for sub-system failures.
Through various fields such as flight mechanics, aircraft design (multiphysics and multi-domain modelling), and automatic control, this theme aims to define methods and algorithms for optimal integrated design, aerodynamic models, structure, propulsion, and environmental models; and study the strong and weak couplings between models.
The resources that are being developed, such as the Multidisciplinary Design Analysis and Optimisation (MDAO) design workshop and the flight demonstrator, are enabling innovation, with applications for the design of the BWB flying wing, distributed propulsion, the design of long-length aircraft, the design of sub-systems (electric de-icing systems, demonstrators), and implementation of a complete Multi-domain Modelling, Simulation, and Analysis workshop under the OpenMDAO framework.
The management of space debris and autonomous missions to asteroids are all issues targeted by this theme, which aims to study future concepts that are typically possible within a timeframe of 15 years or more, such as in-orbit servicing for telecommunications satellites, space traffic management, the architecture of manned bases on the surface of the Moon or Mars, etc.
Through systems engineering and automation, with the help of space systems design software suites integrating the tools already available at DCAS, this theme addresses the following points: Adaptation and/or development of design methods, with particular emphasis on the concept of interface, architecture of large structures for manned exploration missions, formalization of trajectories and attitude control from the launch phases to the rendezvous phases in LEO, GEO and LP orbits.
DCAS is involved in national and European research projects and works with a large number of industrial partners (major groups, SMEs, startups).
Decision and Control Scientific Group - DC
Research Themes
Theme 1: Methods and tools for modelling and controlling aeronautical and space systems and vehicles
- Synthesis of robust control laws for driving vehicles in severe conditions
- Control of aeronautical systems and vehicles meeting flight quality, certification, and energy consumption criteria
- Estimation and control of the flexible modes of high elongation structures
Theme 2: Decision-making under uncertainty, mission planning
- Secure and robust on-line planning for the autonomy of aerospace systems
- Improving the adaptability and safety of multi-agent systems
- Human-centred design of heterogeneous collaborative aerospace systems
Aeronautical Vehicle Design and Flight Dynamics Scientific Group - CADV
Research Themes
- Theme 1: Preliminary aircraft design
- Exploration of innovative aerostructure architectures
- Exploring new propulsion architectures
- Operability and maintainability of new architectures
- Safety and certifiability of new architectures
- Design of electromechanical de-icing systems
- Theme 2: Modelling and assessment of technologies and scenarios for air transport in the context of decarbonisation and transition
- Modelling the air transport system (fleet renewal, use of alternative fuels, economic models)
- Development of climate models
- Assessment of the environmental impact of decarbonisation solutions for air transport over their entire life cycle
Space Systems Design Scientific Group - CSS
- Access to space: physical modelling and design of new-generation liquid rocket engines
- Astrodynamics and mission analysis: modelling and optimisation of trajectories in non-Keplerian environments
- Robotic and manned space exploration combining systems engineering, space system design, on-board autonomy and human factors
- Sustainability of space activities
Human, Systems and Interactions Scientific Group - HSI
- Understanding brain function and human performance
Cognitive performance in stressful situations or during ageing
Massive data analysis applied to brain function
Development of brain-machine interfaces
Design of innovative integrated sensors for monitoring the state of the operator in extreme environments
Sustainable Aviation
DCAS has developed AeroMAPS, an open source tool for modelling transition trajectories for the aviation sector, the result of three years of research within the department. Initially designed under the name CAST, this reference tool can be used to assess the climate impact of aviation, by integrating variables such as traffic volume, energy consumption and the type of fuel used.
Innovative and multidisciplinary, AeroMAPS takes into account all the climatic effects of aviation, beyond CO₂ alone, including contrails and nitrogen oxide emissions. Aimed at research, training and experts and decision-makers in the sector, it helps to inform strategic choices in connection with international commitments to combat climate change. With this work, ISAE-SUPAERO is asserting its active role in the public debate on the future of aviation.
Our Research Projects
- STOL and VTOL control
- Guidance and navigation strategy planning for UAVs in urban environments
- Hybrid hydrogen-powered regional aircraft
- Aviation carbon trajectories
- Design and optimisation of high aspect ratio wings
- Low-consumption electromechanical de-icing systems
- Mitigation of space debris
- Reusable launchers
- Real-time monitoring of human performance
Andre Galli, Smith Heather, Blanc Michel, et al., Lizy-Destrez Stéphanie, Goals and trends in space exploration: An overview of the...
Digital Thread-Based Optimisation Framework for Aeronautical Structures: A Vertical Tail Plane Use Casede Longueville Sébastien, Bouvet Christophe, Bénard Emmanuel, Jézégou Joël, Gourinat Yves, Digital Thread-Based Optimisation Framework for Aeronautical Structures: A Vertical...
Dynamic UAV trajectory optimisation for parcel delivery with integrated third-party risk mitigationAldao, Enrique, Veiga-López, Fernando, Ponzoni Carvalho Chanel Caroline, Watanabe Yoko, González-Jorge, Higinio, Dynamic UAV trajectory optimisation for parcel delivery with...
FIT-SLAM 2: Efficient 3D exploration with Fisher information and traversability-based adaptive roadmapSaravanan Suchetan, Bains Anaïs, Ponzoni Carvalho Chanel Caroline, Vivet Damien, FIT-SLAM 2: Efficient 3D exploration with Fisher information and traversability-based...
Data-driven multifidelity surrogate models for rocket engines injector designZapata Usandivaras Jose Felix, Bauerheim Michaël, Cuenot Bénédicte, Urbano Annafederica, Data-driven multifidelity surrogate models for rocket engines injector design. 2025,...
Our Resources
The vast majority of these resources are managed by the technical group, which develops and implements a range of hardware platforms and software tools:
- Flight simulators (human factors research, flight mechanics training, piloting)
- An aeronautical software suite (flight mechanics, aircraft design, flight tests)
- A space software suite (orbitography, satellite energy subsystem, launchers, ground stations)
- UAVs and UAV systems
- Satellite ground segments (rooms and ground stations for satellite projects)
Certain platforms are used/developed in conjunction with other technical teams:
- The flight test software platform and the flight management software are developed with the Lasbordes flight operations centre
- The autonomous systems room is used and developed with the technical group of the Complex Systems Engineering Department (DISC) at ISAE-SUPAERO
Aeronautical Sector
The DCAS technical group is developing a software suite for teaching and research in the field of aeronautics.
These include tools for simulating aircraft movement (Longisim and Transsim), calculating performance or aiding design (Alcazar), and in-flight training with the TB20 instrumented aircraft (TB20 system). A final piece of software (Activol) provides flight management for the aircraft at the Lasbordes Air Operations Centre.
Flight mechanics: LONGISIM/TRANSIM software
These two software packages are dedicated to the study of the longitudinal and lateral movements of the aircraft. They allow simulations to be carried out according to the type of aircraft and flight characteristics (responses to steps, curves, 3D, etc.).
Aircraft design: “ALCAZAR” software
Alcazar is a software package for the complete study and design of an airliner. Weight estimates, fuselage sizing (number of seats per class, etc.), wing geometry, empennage, thrust settings, etc.
Numerous visualisations allow you to see the results of the design throughout the process.
Flight tests / Flight dynamics: The TB20 System
The “TB20 System” is a software package which, from an instrumented TB20 aircraft (25 parameters in telemetry), enables flight parameters to be displayed in real time or off-line: Flight dynamics teaching (in flight or on the ground), flight tests.
Flight management: ACTIVOL software
ACTIVOL is the software used for the day-to-day management of flights at Lasbordes. Statistics are extracted for the annual activity reports.
In the field of aeronautics, a wide range of equipment is available at the DCAS: Flight simulators (PEGASE, 6MOUV), a drone design workshop, and drone flying platforms.
PEGASE flight simulator
PEGASE: Platform for Experiments on Generic Aircraft Simulation Environment
This simulation platform, halfway between high-end simulation (6-axis training simulators) and individual computer simulation, is ideal for teaching flight mechanics and research into human factors.
This generic simulator can simulate any type of aircraft. The basic model for the activities is the Airbus A300.
Developments are fully managed by the DCAS technical group, which means that the platform can be adapted to any need arising from the scientific teams (research, experimentation, demonstrations, teaching, etc.).
Features
- Controls: Top-of-the-range equipment with pilot/copilot mini-sticks, rudder pedals, A320 throttles + trim wheels, FCU, MCDU.
- EFIS/ECAM A320 cockpit displays: Primary Flight Display, Navigation Display, Engine Warning Display, Flight Control. They are multiplatform and reusable for other projects.
- 3D visualisation: A panoramic 3D visualisation provides a view of the outside world. It comes from the FlightGear open-source simulator, but has been adapted to meet requirements (particularly for the HUD: Head Up Display).
- Movement: A 3-axis hydraulic system reproduces movement (pitch, roll, height).
- Audio server: Alarms, engines, animations (slats and flaps up/down, landing gear, rain, etc.).
6MOUV flight simulator
6MOUV is a single-seat, 3-axis platform, light aircraft (DR400) simulator based on Flight Simulator software.
Drones
Workshop
A workshop dedicated to the final phase of drone design is run at the DCAS.
UAVs
A number of stationary UAVs developed at DCAS have been produced in the workshop (VisionAir, ScolAir, ScanAir). A fixed-wing flying platform is currently being developed (ExpAir, for the ExpeDrone project).
Space Sector
The DCAS technical group is developing a software suite for teaching and research in the space sector.
These include tools for the simulation and design of space systems: SatOrb, SimuSat and SimuLaunch.
SATORB software
SatOrb is a complex multi-satellite, multi-station orbitography and mission analysis software package. It allows 2D and 3D display of satellites and constellations, as well as multiple analyses of access, visibility, coverage, and radio link assessments.
SIMUSAT software
SimuSAT is a software package for simulating a satellite's energy sub-system. The available modules also enable attitude control and simplified simulation of thermal behaviour. This constantly evolving software, combined with Satorb, is a powerful tool for simulating a complete space system.
SIMULAUNCH
Simulaunch is a simulator dedicated to the design of launchers and the study of their trajectory during launch.
DCAS also has space hardware resources: A ground station in Toulouse (UHF/VHF), a ground station in Cayenne (S-band), and a control centre for its nanosatellite projects, which is designed to be simple and generic.
UHF/VHF -T ground station
The ISAE-SUPAERO teams have a ground station for exchanging digital data with the satellite they want, in UHF/VHF, whether in uplink (remote controls) or downlink (telemetry). The station can operate autonomously and collect data from the satellite automatically. A room is dedicated to this ground station in Toulouse.
Ground station (S-band)
ISAE-SUPAERO has had an S-band station since 2000. For technical reasons, it was installed in Cayenne. In cooperation with MIT and RIKEN, it provided a network of ground stations located on the equator to respond to on-board-ground link problems, due in particular to the platform's equatorial orbit.
SCC: Simple Control Center
The control centre manages all the data exchanged between the satellite and the ground segment using lightweight, high-performance software tailored to the university context and state-of-the-art in terms of both data processing and man-machine interface. It is a robust, stable, reusable tool that complies as far as possible with existing European (ECSS) and international (CCSDS) standards.
Directory
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This resource allows you to explore the fields and research projects of our scientists.
Head of the DAEP Department
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Theory, Modelling, and Systems Engineering (ThéMIS) Scientific Group
Our Research Areas
Our mission is to respond to the challenges posed by the design of increasingly integrated, autonomous, and mission-critical systems, by combining theoretical research, modelling methodology, and the implementation of engineering processes.
ThéMIS aims to develop robust and innovative solutions based on an interdisciplinary approach combining modelling, optimisation, and validation. We work with academic and industrial partners to meet the needs of critical sectors and innovate the technologies of tomorrow.
The ThéMIS research group carries out research in the following areas:
Theory
- Preliminary design of complex systems and exploration of the design space
- Architecture and trade-off analysis
- Semantics of models and formal verification and validation (V&V) methods
- System resilience (e.g. identification of obsolescence risks)
- Technology forecasting and roadmapping
Modelling
- Model-based systems engineering (MBSE)
- Links with functional safety analysis (MBSA) and multidisciplinary optimisation (MDAO)
- Model transformation and integration of validation and verification tools
Engineering Process
- Integration of MBSE, product lifecycle management (PLM) and lifecycle analysis (LCA) methodologies
The research carried out by the ThéMIS research group has applications in the following areas:
- Space (ground segment, vehicles, satellites)
- Autonomous vehicles (drones, robots, intelligent cars)
- Complex socio-technical systems (infrastructure management, human-machine interaction)
- Critical embedded systems and cyber-physical systems (safety, reliability and performance in constrained environments)
- Jonathan : Security evaluation of large distributed and reconfigurable systems
- Charles MATHOU: Global methodological framework for safety analysis of UAV systems
- Abdoulaye SARR: Multidisciplinary analysis and optimisation of a hydrogen-powered aircraft
- Charlotte STROBBE: Design of user-centred systems combining MBSE and HSI
- Augustin GALLOIS: Eco-design of a Lunar Habitat
- Ariane BEAUDOIN-BUSSIÈRES : Forecasting for dual technological innovation in strategic ecosystems
- Haochen GAO: Participatory design tools and systemic methods for multimodal air-rail systems
- Valentin MORDEL: Fault tolerance and reliable reconfiguration in an automotive HPC/ZCU architecture
- Maisa CIETTO: Identification and modelling of inefficiencies in the air transportation system
- Sophie LEMOUSSU : A model-based approach for innovative SMEs in the aeronautics industry
- Sébastien SCHWARTZ : Coupling deterministic and non-deterministic simulation for predictive maintenance
- Juan José MONTERO JIMENEZ: Knowledge reuse to improve system architecture for predictive maintenance
- Eric-Guillaume VIDOT: Towards the certification of avionics systems based on machine learning: using mathematical proofs to guarantee reliability
- Anass AKRIM : Prediction of remaining lifetimes of aeronautical components using deep learning approaches
- Ombeline AIELLO: Early validation of system designs using a joint engineering approach based on models and optimisation
- Sophia SALAS CORDERO: Early phases of complex system design: obsolescence considerations from an MBSE perspective
- Eric RAZAFIMAHAZO: A systems engineering approach to the design of multi-use systems on mission inside buildings
- Morgan GAUTHIER: Architectural optimisation of automotive applications on MpSoC components
- Laetitia BORNES: Interactive systems engineering between design science and design as science
Faculty members
Theses in progress
Theses defended
Our Classes
The members of the ThéMIS group are involved in ISAE-SUPAERO’s educational programmes: the general engineering programme, industrial engineering speciality programme by apprenticeship, Master’s degree in Aerospace Engineering (MAE) and various Advanced Master® (AM) programmes.
The group manages the MAE Systems Engineering major (around 30 students/promotion) and the Systems Engineering AM (around 10 students/promotion).
Members of the group are involved in other activities, in particular directing the Systems Doctoral School at the University of Toulouse.
Our Projects
New design, analysis, and qualification methods to ensure drone certification.
Formal verification methods for space systems. Development of the model-checker integrated into ESA's TASTE development platform (https://taste.tools), in collaboration with UGA/Verimag, GMV, and ESA/ESTEC.
Integrated Air Transport System chair with Thalès Group: this sponsorship, research, and teaching chair draws on ISAE-SUPAERO's expertise in optimising the flight operations and systems approach, and on the Thalès Group's expertise in flight avionics, connectivity, and air traffic control.
Our Permanent Members
Head of Themis Group
Thémis Group | Members 2025
Our Partners
Industry Partners
Academic Partners
Directory
Discover the profiles of the 130 faculty members at the Institute who are pioneering research in aeronautics and space.
This resource allows you to explore the fields and research projects of our scientists.
Job Offers
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Learning, Decision, Optimisation (ADO) Scientific Group
Our Research Areas
Our work focuses on decision support systems, from the collection of data to its interpretation, in order to make the best decision.
Our common scientific question is: ‘What are the models and algorithms that lead to a learning or decision-making process?’
To answer this question, the ADO group draws on and contributes to the techniques of artificial intelligence (reinforcement learning, evolutionary algorithms, constraint programming) and industrial engineering (operations research, knowledge management, systems engineering).
The applications of the research carried out within the ADO research group are in the following fields:
- Aeronautics and Space: Earth Observation and Autonomous Vehicles
- Production systems: System configuration and workshop programming
- Industry X.0: Preventive maintenance
Doctoral and post-doctoral students
Researchers
Research areas
Teaching modules
Our Classes
Our research group is heavily involved in ISAE-SUPAERO‘s top-quality educational programmes, both in the engineering cycle curriculum and in the Masters programmes. We are fully committed to teaching, offering courses that combine theory and application, to ensure that students receive an education based on the latest scientific and technological advances.
We encourage and promote participation in research projects to enable our students to develop the practical and methodological skills that are essential in the field of decision support systems.
We are involved in the following modules:
- Third-year Decision Sciences course
- Data and Decision Sciences pathway
- Industrial Engineering pathway
- F-SD320 Supply Chain
- F-SD321 Production
- F-SD322 Modelling and Simulation
- F-SD323 Quality and IS
- F-SD311 Machine Learning
- F-SD312 Big Data
- F-SD313 Digital Eco. Digital
- F-SD314 Case Studies
- F-SD319 Seminars
Our Partners
Head of ADO Group
Directory
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This resource allows you to explore the fields and research projects of our scientists.
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Applied Mathematics (MA) Scientific Group
Our Research Areas
One of the main fields of study, which brings together almost all these themes, is the theoretical and numerical study of problems related to fluid-structure interactions.
These research activities are carried out in collaboration with the major players in Toulouse: The Toulouse Mathematics Institute (Paul Sabatier University-INSA), ONERA and the Clément Ader Institute (ICA), as well as with other national and international partners.
The Applied Mathematics (MA) research group comprises seven faculty members and one research engineer.
Contributions are mainly made to the following research themes:
*The division presented below is not strict: Interactions exist.
In this research area, we are interested in various aspects of the control and stabilisation or stability of solutions to partial differential equations. To be more precise:
- Control of partial differential equations
- Fluid-Structure Interaction
- Hamiltonian systems with interaction ports (pHS)
The idea behind interaction port Hamiltonian systems is to describe the dynamics of a system using the physical energy of the system (called the Hamiltonian).
In particular, this makes it possible to deal with non-linearities (non-quadratic Hamiltonian) in general. Analysis of the associated Cauchy problem is still an active research topic in the case of infinite-dimensional systems (typically non-linear partial differential equations).
Interaction ports classically consist of co-located control and observation (among other things), enabling different pHs to be coupled. The resulting system is still a pH. There are algebraic structures subordinate to pHs: Dirac structures.
Numerical simulation of pHs calls for special numerical methods to preserve the Hamiltonian (or, more precisely, the existence of a Dirac structure associated with the discretized system).
It should also be noted that closed-loop stabilisation is easily obtained in pHs, and that they also allow, at least in finite dimension, constraints to be taken into account in the form of algebraic equations coupled to the dynamical system.
- Fractional and Diffusive Differential Systems (SDF)
- Well-Posed Linear Systems (WPLS)
This area of research focuses on numerical optimisation and multidisciplinary optimisation in the context of pre-project design. To be more precise:
- Development and analysis of optimization algorithms (deterministic and stochastic)
- Solving large linear systems and preconditioning
- Uncertainty propagation (UQ)
- Sensitivity analysis
- Substitution models
- High-Performance Computing (HPC)
This area of research focuses on the application of probability and statistics to practical problems encountered by industry. To be more precise:
- Performance analysis of communication networks
- Sensitivity analysis
- Random trees
Our Partners
Head of MA Group
Directory
Discover the profiles of the 130 faculty members at the Institute who are pioneering research in aeronautics and space.
This resource allows you to explore the fields and research projects of our scientists.
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Design and Analysis of Critical Systems (CASC) Scientific Group
Our Research Areas
The Critical Systems Analysis and Design (CASC) group focuses on methods and tools to support systems engineering, with the following objectives:
- To extend the state of the art in terms of software dependability, from the design of the initial model to the hardware target, as well as in the definition and use of support tools for formal simulation/verification.
- To contribute to the definition and formal modelling of new system architectures, and to the integration of new software functionalities such as those arising from AI.
The CASC group covers several facets of software-intensive system engineering: design, verification, and validation of critical systems, deployment on hardware targets, and, finally, distributed and real-time simulation.
Our contributions are applied to aeronautics and space, but also more broadly to embedded and cyber-physical systems. These contributions are presented through publications on OpenScience and software, some of which can be freely distributed.
The CASC group is organised around two research themes:
The Formal Methods and Dedicated Languages theme is concerned with the formal semantics of programming languages as well as programs and their specifications, applied particularly to languages adapted to the design of critical embedded systems.
The use of formal methods (programme proofs, SAT/SMT methods, correction by construction, etc.) for the rigorous design of avionics functions can be applied to the various stages in the design and implementation of a product: architecture consistency verification, proof of correct operation of model transformation/code generation tools, and proof of correctness of the application code to be embedded.
The study of dedicated languages (synchronous reactive, probabilistic, etc.) and their semantic aspects will ensure that programmes can be embedded for the implementation of avionics functions, for example, taking into account the strong requirements and constraints of the field, both in terms of computing resources and the implementation of advanced AI-based functions (neural networks or learning by Bayesian inference).
The Architecture and Simulation of Cyber-Physical Systems theme focuses on the V&V stages of critical systems, particularly in conjunction with the PRISE platform.
- New avionics architectures: taking into account new processor and network paradigms and their safe integration into an avionics platform (SMARTIES project)
- Embeddability of applications on hybrid architectures (CPU, GPU and FPGA), in particular neural networks and their complex decision tasks
- Systems simulation based on state-of-the-art tools
- Real-time distributed simulation, through the implementation of the HLA standard by the CERTI middleware developed in partnership with ONERA. CERTI implements versions 1.3 and 1516 of the HLA simulation standard.
- Interoperability and coupling of simulation models for cyber-physical systems, with the Ptolemy-HLA tool. This distributed co-simulation environment couples two open-source tools, Ptolemy II and CERTI/HLA. It takes advantage of Ptolemy's calculation models and the HLA standard for interoperability and deterministic distribution of simulations.
Our Team
Permanent Team Members
- Jannette Cardoso (HdR)
- Jean-Baptiste Chaudron
- Arnaud Dion
- Fabrice Frances
- Christophe Garion
- Christine Tasson (HdR)
- Xavier Thirioux (HdR)
7 PhD Students
Head of CASC Group
Directory
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This resource allows you to explore the fields and research projects of our scientists.
Job Offers
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Connected Systems (SysCo) Scientific Group
Our Research Themes
To meet the Institute’s teaching needs, the SYSCO research team’s skills cover all the fields of application of networks and connected systems in the various aerospace contexts.
The global vision developed by the team has made it possible to identify three major research themes on which research efforts have been focused for several years:
- Satellite networks: Secure and deterministic data transmission
- Embedded systems and networks: Design and performance analysis of embedded systems and networks subject to deterministic and security constraints
- Distributed systems: Reliable and secure large-scale distributed storage
Each teacher-researcher contributes to at least two of the team’s three research themes, which makes it possible to generate multiple collaborations and cross-disciplinary contributions in addition to results focused on one area.
In addition, several collaborations with members of the department’s other research groups and other departments (notably DEOS) are also prolific.
This research work has been put to good use in a number of ways over the last 5 years:
- Supervision of more than twenty doctoral and post-doctoral students
- Publication of around a hundred scientific papers and international patents
- Setting up three research platforms: Ireal/Satenet for satellite networks, Blockchain 4 UAV for distributed systems, and Factoring for embedded networks
- Participation in more than a dozen research projects with industrial and academic partners, including regional projects, ANR projects, industrial projects (TAS, Thales Avionics, AIRBUS), CNES R&T, and projects with the Institut de Recherche et de Technologie (IRT) Antoine de Saint-Exupéry.
Our Scientific Challenges
The main scientific issues that we are considering in order to advance the state of the art in our work in each of these research areas are:
For Satellite Networks
- Large-scale multi-orbit dynamic system and its heterogeneity with terrestrial networks
- Improving the security of communication protocols using post-quantum cryptography
- Definition and integration of secure routing with deterministic QoS guarantees (throughput, delay)
For Embedded Networks and Systems
- Heterogeneous hardware architectures and a variety of access control mechanisms
- Joint SW and HW approach for deterministic execution on multicore/manycore
- Definition and analysis of scheduling strategies for embedded applications
- Definition and analysis of security mechanisms adapted to real-time networks
- Methods for evaluating the security/performance trade-off
In Distributed Systems
- Ensuring scalability, data integrity, and mitigation of cyber-security risks
- Implementation of cybersecurity mechanisms and post-quantum cryptography
- Definition of 'zero knowledge' mechanisms for blockchains and peer-to-peer networks
- Integration of erasure codes to ensure the reliability and integrity of distributed storage
Team Members
Ahlem MIFDAOUI (Team Leader)
- Real-time and satellite networks
- Routing, QoS
- Cryptography and Cybersecurity
- Blockchains
- Cryptography and reliability
- Distributed Systems/Blockchains
- Cryptography and Cybersecurity, Blockchains
- Satellite networks, Routing, QoS
*Head of DISC
- Real-time Networks and Systems
- Dependability, OS
- Distributed Systems/Blockchains
- Dependability
Head of SysCo Group
Our Partners
Academic Partners
At the National Level
At the International Level
State and Industrial Partners
Directory
Discover the profiles of the 130 faculty members at the Institute who are pioneering research in aeronautics and space.
This resource allows you to explore the fields and research projects of our scientists.
Job Offers
Check out the vacancies for scientific staff in the research department
Thesis Offers
Check out the research department's thesis and post-doctorate vacancies
Internship Opportunities
Check out the Research Department's internship opportunities!