Control of an electro-hydrostatic actuation system for the nose landing gear of an "all electric aircraft"
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
-
In: Recent Advances in Aerospace Actuation Systems and Components 2004, Toulouse, November 24-26, 2004
- Classification
-
Ingenieurwissenschaften und Maschinenbau
- Event
-
Veröffentlichung
- (where)
-
Hamburg
- (who)
-
Universitätsbibliothek der Technischen Universität Hamburg-Harburg
- (when)
-
2004
- Creator
- URN
-
urn:nbn:de:gbv:830-opus-2731
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
14.08.2025, 11:00 AM CEST
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Greißner, Carsten
- Carl, Udo B.
- Universitätsbibliothek der Technischen Universität Hamburg-Harburg
Time of origin
- 2004
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Comparison of Electro-Hydraulic and Electro-Mechanic Landing Gear Actuation for Light VTOL Aircraft
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Simulation of landing gear dynamics and brake-gear interaction
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Hierarchical Optimization of Landing Performance for Lander with Adaptive Landing Gear
Advanced conceptual design methods for aircraft landing gears
Main Landing Gear Operation powered by Multifunctional High-Lift PCUs
The landing gear system in multi-machine Hybrid Event-B
Landing Gear Design and Assessment Methodology in the AVACON Project
Design and analysis of semi-active landing gears for transport aircraft
Preliminary Weight Estimation for different Actuator Types for Landing Gear Retraction
Model-Based Loads Observer Approach for Landing Gear Remaining Useful Life Prediction
Comparison of Electro-Hydraulic and Electro-Mechanic Landing Gear Actuation for Light VTOL Aircraft
Unlocking a nose landing gear in different flight conditions: folds, cusps and a swallowtail
Simulation of landing gear dynamics and brake-gear interaction
Simulation of landing gear dynamics and brake-gear interaction
Hierarchical Optimization of Landing Performance for Lander with Adaptive Landing Gear
Advanced conceptual design methods for aircraft landing gears
Main Landing Gear Operation powered by Multifunctional High-Lift PCUs
The landing gear system in multi-machine Hybrid Event-B
Landing Gear Design and Assessment Methodology in the AVACON Project
Design and analysis of semi-active landing gears for transport aircraft
Preliminary Weight Estimation for different Actuator Types for Landing Gear Retraction