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Wednesday, May 30, 2018
| Time | Event | |
| 07:30 - 09:00 | Registration - Registration | |
| 09:00 - 09:15 | Welcome - C. CHASSOT, director of research, INSA | |
| 09:15 - 09:45 | Session 1. AIRBUS Research and perspectives for aircraft control actuation | |
| 09:45 - 10:15 | Session 1. Electro-hydraulic system architectures for more electric aircraft - Comparison of central and zonal power packages | |
| 10:15 - 10:45 | Session 1. Spoiler and flap rotary EM actuation (REMA) implementation on a recently certified business jet | |
| 10:45 - 11:15 | Coffee break and poster display | |
| 11:15 - 11:45 | Session 2. Pseudo direct drive electrical machine for primary flight control surface actuation | |
| 11:45 - 12:15 | Session 2. A model-based systems engineering approach for efficient flight control system architecture variants modelling in conceptual design | |
| 12:15 - 12:45 | Session 2. State and development of actuation system and component in China | |
| 12:45 - 14:00 | Lunch | |
| 14:00 - 14:30 | Session 3. Reliability of the electronics for actuation? | |
| 14:30 - 15:00 | Session 3. Linear EMA HM using oil detection | |
| 15:00 - 15:30 | Session 3. First practical evaluation of a complete Fail-safe and 100% fault-tolerant inverter for critical load in aerospace application | |
| 15:30 - 16:00 | Coffee break and poster display | |
| 16:00 - 16:30 | Session 4. Electromechanical actuation for landing gear application: A case study on end-stroke impact in case of high speed free-fall emergency extension | |
| 16:30 - 17:00 | Session 4. Physical modeling and bond graph combined approach to guide failure analysis in an aircraft hydraulic brake system | |
| 17:00 - 17:30 | Session 4. Overview of Integrated Self-Powered Brake System for aircrafts |
Thursday, May 31, 2018
| Time | Event | |
| 07:30 - 08:30 | Registration - Registration | |
| 08:30 - 09:00 | Session 5. Virtual testing of aircraft hydraulic systems | |
| 09:00 - 09:30 | Session 5. Automated measurement of backlash and stiffness in electro-mechanical flight control actuation | |
| 09:30 - 10:00 | Session 5. Methodologies and test-rig configurations for the experimental improvement of aerospace flight control actuation systems | |
| 10:00 - 10:30 | Session 5. Flight control system architecture comprehensive evaluation based on electrical actuators for more electric aircraft | |
| 10:30 - 11:00 | Coffee break and poster display | |
| 11:00 - 11:30 | Session 6. EMADEF: a fully comprehensive analytical tool for the initial design of electro-mechanical servo-actuators for primary flight controls | |
| 11:30 - 12:00 | Session 6. Optimization of primary flight control actuation system using parametric sizing models of actuators, power electronics and structural analysis | |
| 12:00 - 12:30 | Session 6. Power cycling reliability and thermal performances of SiC power modules | |
| 12:30 - 14:00 | Lunch | |
| 14:00 - 14:30 | Session 7. Challenges of ball screw lifetime calculation in primary flight control applications | |
| 14:30 - 15:00 | Session 7. High fidelity model for efficiency calculation of ball screws for flight control actuators | |
| 15:00 - 15:30 | Session 7. A novel industry-oriented EMA model for ball screw optimised design including motor torque response and friction | |
| 15:30 - 16:00 | Coffee break and poster display | |
| 16:00 - 16:30 | Session 8. Development of an innovative piezo actuated flow servovalve with additive manufacturing body | |
| 16:30 - 17:00 | Session 8. The hydraulic infinite linear actuator applied to a high lift system | |
| 17:00 - 17:30 | Session 8. Implications of the use of flux-switching motors for aerospace actuation systems | |
| 18:30 - 20:00 | Private visit of Toulouse Museum - Private visit of Toulouse Museum | |
| 20:00 - 23:00 | Aperitive and banquet |
Friday, June 1, 2018
| Time | Event | |
| 08:30 - 09:00 | Session 9. Fault-tolerant control system of the directional runway dynamics of small aircrafts with hydraulic differential brakes | |
| 09:00 - 09:30 | Session 9. Aircraft control using actuator current | |
| 09:30 - 10:00 | Session 9. Research on the operating modes and force fighting of hybrid actuation system based on EHA/SHA | |
| 10:00 - 10:30 | Session 9. Identifying enhancement potentials of actuation systems using a criticality index | |
| 10:30 - 11:00 | Coffee break | |
| 11:00 - 11:30 | Session 10. Highly responsive micro-EMA with regenerative recovery | |
| 11:30 - 12:00 | Session 10. Active/active aileron EMA system with optimised power supply architecture | |
| 12:00 - 12:30 | Session 10. Design considerations and test of the flight control actuators for a demonstrator for an unmanned freight transportation aircraft | |
| 12:30 - 12:45 | Conference closure - J-C. Maré | |
| 14:00 - 17:30 | Tutorial. Introduction to optimization of actuation systems with opensource tools. Special registration required. Location: INSA - M. Budinger | |
| 14:00 - 17:30 | Tutorial. Virtual prototyping of mechanical transmission of aerospace actuators. Special registration required. Location: INSA - J-C. Maré |
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