| People | Locations | Statistics |
|---|---|---|
| Seuring, Stefan |
| |
| Nor Azizi, S. |
| |
| Pato, Margarida Vaz |
| |
| Kölker, Katrin |
| |
| Huber, Oliver |
| |
| Király, Tamás |
| |
| Spengler, Thomas Stefan |
| |
| Al-Ammar, Essam A. |
| |
| Dargahi, Fatemeh |
| |
| Mota, Rui |
| |
| Mazalan, Nurul Aliah Amirah |
| |
| Macharis, Cathy | Brussels |
|
| Arunasari, Yova Tri |
| |
| Nunez, Alfredo | Delft |
|
| Bouhorma, Mohammed |
| |
| Bonato, Matteo |
| |
| Fitriani, Ira |
| |
| Autor Correspondente Coelho, Sílvia. |
| |
| Pond, Stephen |
| |
| Okwara, Ukoha Kalu |
| |
| Toufigh, Vahid |
| |
| Campisi, Tiziana | Enna |
|
| Ermolieva, Tatiana |
| |
| Sánchez-Cambronero, Santos |
| |
| Agzamov, Akhror |
|
Denti, Eugenio
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (10/10 displayed)
- 2017Wind identification via Kalman filter for aircraft flow angles calibrationcitations
- 2014Simulation of an All-Electric Flight Control System for the Evaluation of Power Consumption
- 2013Development of a fault tolerant EMAS for MALE UAV
- 2013Reconfiguration control laws for fault-tolerant hydraulic actuators of fly-by-wire helicopters
- 2013Evaluation of the Avoiding Strategies for a Prototype Sense and Avoid System of Small Size UAVs
- 2013Suitability of using closed-loop current controls on EMAS for aircraft applications
- 2013Architecture definition and safety assessment of the flight control system for a light rotary-wing UAV
- 2013Co-Simulation for Design, Optimization and Analysis of All-Electric Aircraft Systems
- 2007Robust force control in a hydraulic workbench for flight actuatorscitations
- 2006Air Data Computation in Fly By Wire Flight Control Systems
Places of action
| Organizations | Location | People |
|---|
conferencepaper
Suitability of using closed-loop current controls on EMAS for aircraft applications
Abstract
The paper deals with the control design and the performance analysis of Electro-Mechanical Actuators (EMAs) for aircraft application. In particular, the study is focused on evaluating the suitability of using the closed-loop current controls, depending on the application the EMA is addressed for. Current loops, implying additional sensors and digital processing at high frequency rates, significantly impact on EMA development costs, and their use must be settled by correctly balancing related advantages and drawbacks. In the work, two EMA applications are analysed via modelling and simulation: position-controlled (e.g. flight control) and speed-controlled (e.g. landing gears, flaps, airbrakes). For both cases, two control strategies are developed, by implementing or not the closed-loop control on the motor currents. The dynamic behaviour of the EMA solutions are thus characterised in terms of command tracking and power absorption, highlighting and discussing the effects of the current loops on actuator performances.
Topics
Search in FID move catalog