Options
Control of an electro-hydrostatic actuation system for the nose landing gear of an "all electric aircraft"
Citation Link: https://doi.org/10.15480/882.208
Publikationstyp
Conference Paper
Date Issued
2004
Sprache
English
Author(s)
Institut
TORE-DOI
Citation
Recent Advances in Aerospace Actuation Systems and Components 2004, Toulouse, November 24-26, 2004
The EU research Project Power Optimised Aircraft (POA) investigates the approach to replace primary hydraulic supply by extended electric power systems towards a More or All Electric Aircraft. This contribution presents an electrically powered actuation system for nose landing gears using an EHA (electrohydrostatic actuator) approach. One motor pump unit supplies door and gear actuation as well as the steering system. Different control strategies for the individual actuators are introduced. The effects of different control strategies are shown by simulation results.
Subjects
Electro-Hydrostatic Actuator (EHA)
Nose Landing Gear
All Electric Aircraft
Power Optimised Aircraft (POA)
Loading...
Name
208_3.pdf
Size
824.59 KB
Format
Adobe PDF