Fernando, Bernhard (2010) Modelling of a Steerable Main Landing Gear and Development of a Crosswind Landing Assistance System. DLR-Interner Bericht. DLR-IB 111-2010/07, 101 S.
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The intention of this work was to investigate whether a steerable main landing gear combined with a crosswind landing technique without de-crab would enhance the saftey of flight and reduce the pilot's workload. The main idea is to align all landing gears with the runway heading in order to enable a touchdown while maintaining a crab angle, which is needed to counteract the crosswind force. The critical de-crab manoeuvre - i.e. alignin the aircraft with the runway heading - can be performed later, when the aircraft is settled aerodynamically stable on the ground and no danger of a sudden rolling motion or an uncontrallable wind drift exist.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Modelling of a Steerable Main Landing Gear and Development of a Crosswind Landing Assistance System|
|Number of Pages:||101|
|Keywords:||Development of Steerable Main Landing Gears, Gear Modelling, Crosswind Landing Assistance System, steerable main landing gear, Pilot-in-the-Loop Simulations|
|Institution:||FH Joanneum GmbH|
|HGF - Research field:||other|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Systems & Cabin|
|Institutes and Institutions:||Institute of Flight Systems > Flight Dynamics and Simulation|
|Deposited By:||Tanja Bracke|
|Deposited On:||10 Mar 2010 14:13|
|Last Modified:||10 Mar 2010 14:13|
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