Patents Assigned to DLR Deutsches Zentrum fuer Luft- und Raumfahrt e.V.
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Patent number: 8456355Abstract: A method is suggested for robust estimation of a subset of carrier phase integer ambiguities for precise ionospheric delay estimation. The advantages of this method are the precise estimation of receiver and satellite biases, an increase in the number of reliably fixable ambiguities, and an improved accuracy for the ionospheric delay estimation.Type: GrantFiled: October 8, 2010Date of Patent: June 4, 2013Assignee: DLR Deutsches Zentrum für Luft- und Raumfahrt e.V.Inventors: Patrick Henkel, Victor Gomez
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Patent number: 8451168Abstract: A new method for bias estimation on multiple frequencies with a Kalman filter is proposed. It consists of four steps: First, a least-squares estimation of ranges, ionospheric delays, ambiguities, receiver phase biases and satellite phase biases is performed. The code biases are absorbed in the ranges and ionospheric delays, and a subset of ambiguities is mapped to the phase biases to remove linear dependencies between the unknown parameters. In a second step, the accuracy of the bias estimates is efficiently improved by a Kalman filter. The real-valued a posteriori ambiguity estimates are decorrelated by an integer ambiguity transformation to reduce the time of ambiguity resolution. Once the float ambiguities have sufficiently converged, they are fixed sequentially in a third step. Finally, a second Kalman filter is used to separate the receiver and satellite code biases and the tropospheric delays from the ranges.Type: GrantFiled: December 9, 2010Date of Patent: May 28, 2013Assignee: DLR Deutsches Zentrum für Luft- und Raumfahrt e.V.Inventors: Patrick Henkel, Zhibo Wen, Christoph Guenther
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Patent number: 8439307Abstract: The present invention provides a fuselage structure for an aircraft or spacecraft with an outer skin. The fuselage structure comprises a rib element for stiffening the outer skin and ad cross member element. Here the rib element is bent in the shape of an arc to correspond to an inner contour of the outer skin. The cross member element connects two arc sections of the rib element transversely to each other. The cross member element has a higher strength than the rib element. From another point of view the invention provides an aircraft with such a fuselage structure.Type: GrantFiled: December 15, 2009Date of Patent: May 14, 2013Assignees: Airbus Operations GmbH, DLR-Deutsches Zentrum fuer Luft- und Raumfahrt e.V.Inventors: Philipp Westphal, Wolf-Dietrich Dolzinski, Thorsten Roming, Thorsten Schroeer, Dieter Kohlgrueber, Marius Luetzenburger
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Patent number: 8188913Abstract: A method for estimating satellite-satellite single difference biases is described. The method uses an ionosphere-free mixed code-carrier combination of maximum ambiguities discrimination defined at the ration between wavelength and noise standard deviation. The accuracy of the biases estimation is further improved by an additional ionosphere-free mixed code-carrier combination of time-difference measurement that is uncorrelated with the first combination. Finally, an alternative method is based on a combination of carrier signals in a common frequency band which allows estimating the biases individually.Type: GrantFiled: October 22, 2010Date of Patent: May 29, 2012Assignee: DLR Deutsches Zentrum für Luft- und Raumfahrt e.V.Inventor: Patrick Henkel
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Patent number: 7274132Abstract: An electromechanical functional module and associated process for production thereof, which includes at least one transducer, at least one upper fiber cover layer, which is nonconducting and is positioned over the at least one transducer having a first electrode and a second electrode, at least one lower fiber cover layer, which is nonconducting and is positioned below the at least one transducer, at least one fiber interlayer, which is nonconducting with at least one cut-out for accommodating the at least one transducer, at least one upper electric contract strip that is integrally connected to the at least one upper fiber cover layer and in contact with the first electrode of the at least one transducer, and at least one lower electric contract strip that is integrally connected to the at least one lower fiber cover layer and in contact with the second electrode of the at least one transducer, wherein the at least one upper fiber cover layer, the at least one lower fiber cover layer and the at least one traType: GrantFiled: July 18, 2005Date of Patent: September 25, 2007Assignee: DLR Deutsches Zentrum fuer Luft und Raumfahrt E.V.Inventor: Peter Wierach
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Publication number: 20050248237Abstract: An electromechanical functional module and associated process for production thereof, which includes at least one transducer, at least one upper fiber cover layer, which is nonconducting and is positioned over the at least one transducer having a first electrode and a second electrode, at least one lower fiber cover layer, which is nonconducting and is positioned below the at least one transducer, at least one fiber interlayer, which is nonconducting with at least one cut-out for accommodating the at least one transducer, at least one upper electric contract strip that is integrally connected to the at least one upper fiber cover layer and in contact with the first electrode of the at least one transducer, and at least one lower electric contract strip that is integrally connected to the at least one lower fiber cover layer and in contact with the second electrode of the at least one transducer, wherein the at least one upper fiber cover layer, the at least one lower fiber cover layer and the at least one traType: ApplicationFiled: July 18, 2005Publication date: November 10, 2005Applicant: DLR Deutsches Zentrum fuer Luft- und Raumfahrt e.V.Inventor: Peter Wierach
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Patent number: 6930439Abstract: An electromechanical functional module and associated process for production thereof, which includes at least one transducer, at least one upper fiber cover layer, which is nonconducting and is positioned over the at least one transducer having a first electrode and a second electrode, at least one lower fiber cover layer, which is nonconducting and is positioned below the at least one transducer, at least one fiber interlayer, which is nonconducting with at least one cut-out for accommodating the at least one transducer, at least one upper electric contact strip that is integrally connected to the at least one upper fiber cover layer and in contact with the first electrode of the at least one transducer, and at least one lower electric contact strip that is integrally connected to the at least one lower fiber cover layer and in contact with the second electrode of the at least one transducer, wherein the at least one upper fiber cover layer, the at least one lower fiber cover layer and the at least one transType: GrantFiled: October 18, 2001Date of Patent: August 16, 2005Assignee: DLR Deutsches Zentrum fuer Luft- und Raumfahrt e.V.Inventor: Peter Wierach
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Publication number: 20020047496Abstract: An electromechanical functional module and associated process for production thereof, which includes at least one transducer, at least one upper fiber cover layer, which is nonconducting and is positioned over the at least one transducer having a first electrode and a second electrode, at least one lower fiber cover layer, which is nonconducting and is positioned below the at least one transducer, at least one fiber interlayer, which is nonconducting with at least one cut-out for accommodating the at least one transducer, at least one upper electric contract strip that is integrally connected to the at least one upper fiber cover layer and in contact with the first electrode of the at least one transducer, and at least one lower electric contract strip that is integrally connected to the at least one lower fiber cover layer and in contact with the second electrode of the at least one transducer, wherein the at least one upper fiber cover layer, the at least one lower fiber cover layer and the at least one traType: ApplicationFiled: October 18, 2001Publication date: April 25, 2002Applicant: DLR Deutsches Zentrum fuer Luft-und Raumfahrt e.V.Inventor: Peter Wierach