Greiner-Perth, Christian (2010) Documentation of concept, algorithms, simulation and test results for failure tolerant control algorithms. DLR-Interner Bericht. DLR-IB 111-2010/38, 21 S.
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The purpose of this document is the description of concept, algorithms and simulation results for a failure tolerant control applied to parachute load systems. In detail, it is the goal to detect actuator failures occurring during flight and reconfigure the guidance and control system in a way that a precise landing is still possible. The document summarizes the results of a feasibility study to demonstrate model based failure detection for selected actuator faults of a steerable parachute system. The reconfiguration of guidance-, navigation-, control- algorithms (GNC) under faulty conditions is also presented.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Documentation of concept, algorithms, simulation and test results for failure tolerant control algorithms|
|Number of Pages:||21|
|Keywords:||FASTWing CL, Parachute system, Failure Detection, Reconfiguration, FDIR|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|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 > Unmanned Aircraft|
|Deposited By:||Christian Greiner-Perth|
|Deposited On:||28 Oct 2010 16:44|
|Last Modified:||28 Oct 2010 16:44|
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