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    CONFIGURABLE INPUT/OUTPUT PROCESSOR
    82.
    发明公开
    CONFIGURABLE INPUT/OUTPUT PROCESSOR 有权
    可配置的I / O处理器

    公开(公告)号：EP2705426A4

    公开(公告)日：2014-11-12

    申请号：EP11865026

    申请日：2011-05-06

    Applicant: SAAB AB

    Inventor： HÅKEGÅRD JAN ,  DANIELSSON TORKEL ,  GRIPSBORN ANDERS

    IPC: G06F9/44 ,  G06F9/54

    CPC classification number: G06F3/002 ,  H04L67/12 ,  H04W4/005

    Abstract: The invention pertains to a configurable input/output processing device, a method for configuring the configurable input/output processing device and a computer program product for performing the steps of the method. The configurable input/output processing device (6) is arranged to control data traffic associated to a distributed avionics control system comprising a plurality of processing nodes interconnected in a network (2), wherein each of the plurality of processing nodes is connected to the network via at least one of said configurable input/output processing device. The configurable input/output processor comprise first instructions (CCR), said first instructions comprising processing information for the at least one input/output processing device and being independent of a current configuration of the distributed avionics control system and second instructions (SCT), said second instructions being dependent on the current configuration of the distributed avionics control system.

    OBJECT-FOCUSSED DECISION SUPPORT
    84.
    发明公开
    OBJECT-FOCUSSED DECISION SUPPORT 审中-公开
    OBJECT FOCUSED决策支持

    公开(公告)号：EP2791698A1

    公开(公告)日：2014-10-22

    申请号：EP11877292.0

    申请日：2011-12-16

    Applicant: SAAB AB

    Inventor： LUNDQVIST, Anders ,  KENSING, Vibeke

    IPC: G01S13/78

    CPC classification number: F41H11/00 ,  F41G9/002 ,  G01S7/36 ,  G01S7/40 ,  G01S13/78 ,  G01S13/86 ,  G01S13/87 ,  G01S2013/0281

    Abstract: The invention relates to a method for decision support of a combat object (1 ) in a combat situation comprising the steps of: a) detecting (3) an enemy object (2) such that a plurality of characteristic parameters of the enemy object (2) is determined, b) calculating (4) at least one quality factor for at least one combat sensor of the combat object (1 ), wherein each quality factor is adapted for indicating identification ability of a combat sensor, and calculating (4) at least one signature factor for at least one enemy sensor of the enemy object (2) based on a predetermined model, wherein each signature factor is adapted for indicating identification ability of an enemy sensor, c) allocating (5) each quality factor calculated in the previous step b) to each combat sensor and allocating (5) each signature factor calculated in the previous step b) to each enemy sensor, and d) controlling (6) each combat sensor against the enemy object (2) based on the result of the previous step c). In this way, support for the pilot on a target-oriented basis is provided in order to make a quick and efficient decision in a combat situation.

    A METHOD AND AN APPARATUS FOR IMAGE-BASED NAVIGATION
    86.
    发明公开
    A METHOD AND AN APPARATUS FOR IMAGE-BASED NAVIGATION 审中-公开
    VERFAHREN UND VORRICHTUNGFÜRBILDBASIERTE NAVIGATION

    公开(公告)号：EP2622573A4

    公开(公告)日：2014-05-21

    申请号：EP10857956

    申请日：2010-10-01

    Applicant: SAAB AB

    Inventor： MODÉN ANDERS

    IPC: G06T7/00 ,  G06T7/20

    CPC classification number: G06T7/2033 ,  G06T7/246 ,  G06T7/285 ,  G06T7/77 ,  G06T2207/10012 ,  G06T2207/20076 ,  G06T2207/30244

    Abstract: A method and apparatus for determining position and orientation enabling navigation of an object using image data from at least a first and a second 2D image from at least one camera mounted on said object. The method comprises the steps of: correcting images from one or several cameras and from at least a first and a second 2D image for their respective radial distortion and other measurable effects which result in poor image precision; matching 2D image items in and between at least a first and second 2D image; calculating a fundamental matrix by using correlated image points from at least a first and a second 2D image; calculating and extracting estimated first rotation and translation values from the fundamental matrix using single value decomposition (SVD) based on information from at least a first and a second 2D image; iterating more accurate final rotation and translation values by using the LevenBerg-Marquard algorithm and determining the position and orientation of said object.

    Abstract translation: 一种用于确定使用来自安装在所述对象上的至少一个相机的至少第一和第二2D图像的图像数据来导航对象的位置和方向的方法和装置。 该方法包括以下步骤：从一个或多个相机以及至少第一和第二2D图像中校正图像，以获得它们各自的径向失真和其它可测量的影响，这导致图像精度差; 在至少第一和第二2D图像之中和之间匹配2D图像项目; 通过使用来自至少第一和第二2D图像的相关图像点来计算基本矩阵; 基于来自至少第一和第二2D图像的信息，使用单值分解（SVD）从基本矩阵计算和提取估计的第一旋转和平移值; 通过使用LevenBerg-Marquard算法迭代更准确的最终旋转和平移值，并确定所述对象的位置和方向。

    A DOUBLE-CURVED COVER FOR COVERING A GAP BETWEEN TWO STRUCTURAL PORTIONS OF AN AIRCRAFT
    89.
    发明公开
    A DOUBLE-CURVED COVER FOR COVERING A GAP BETWEEN TWO STRUCTURAL PORTIONS OF AN AIRCRAFT 有权
    带双曲线从头到尾：两种结构的飞机部件的间隙

    公开(公告)号：EP2720940A1

    公开(公告)日：2014-04-23

    申请号：EP11867841.6

    申请日：2011-06-16

    Applicant: Saab AB

    Inventor： BJERKEMO, Jakob

    IPC: B64C7/00 ,  B64C1/14 ,  B64C25/16 ,  E04B1/68

    CPC classification number: B64D45/02 ,  B64C7/00 ,  B64C2025/003

    Abstract: The present invention regards a cover for covering a gap (2) between a first structural portion (3, 3 ') and a second structural portion (5, 5') of an aerial vehicle (29, 41 ), the cover (1, 25) comprises a first attachment section (9), attachable to the first structural portion (3, 3'), and a second flexible section (11) for covering the gap (2), the second flexible section (11) includes an abutment portion ( 13) for abutting against the second structural portion (5, 5 ') in an operating state. The abutment portion (13) in an unloaded state forms an undulating shape (U) having troughs (15) and crests (17) extending along a curved plane, the curvature of which essentially corresponds with the curvature (C) of the second structural portion's (5, 5') surface (6, 27), wherein the troughs (15) are provided for engagement with said surface (6, 27) in said operating state in such way that they tend to be flatten out and propagate over said surface (6, 27) pressing down neighbouring crests ( 17) towards said surface (6, 27) for providing a close fit between the cover (1, 25) and the second structural portion (5, 5').

    DISTRIBUTED AVIONICS SYSTEM AND METHOD FOR BACKUP HANDLING IN AN AVIONICS SYSTEM
    90.
    发明公开
    DISTRIBUTED AVIONICS SYSTEM AND METHOD FOR BACKUP HANDLING IN AN AVIONICS SYSTEM 有权
    分布式航空电子系统和用于在航空电子系统中进行备用处理的方法

    公开(公告)号：EP2710473A1

    公开(公告)日：2014-03-26

    申请号：EP11865594.3

    申请日：2011-05-17

    Applicant: SAAB AB

    Inventor： DANIELSSON, Torkel ,  HÅKEGÅRD, Jan ,  GRIPSBORN, Anders

    IPC: G06F11/20

    CPC classification number: G06F11/2041 ,  G06F11/143 ,  G06F11/203 ,  G06F11/2035 ,  G06F11/2043

    Abstract: The present invention relates to a distributed avionics system (100, 500) having a plurality of computer nodes arranged to execute a plurality of partitions/applications (P1, P2, P3, P4, P5, P6). The distributed avionics system comprises reconfiguration means (332) arranged to reconfigure the distributed avionics system upon detection of failure in at least one of the computer nodes. Each partition/application is associated to a application/partition availability level. The reconfiguration means are arranged to reconfigure the distributed avionics system based on the partition/application availability levels of the partition/applications (P1, P2, P3, P4, P5, P6). The present invention further relates to a method for back-up handling in a distributed avionics system having a plurality of computer nodes (A, B, C).

    Abstract translation: 本发明涉及具有被布置成执行多个分区/应用（P1，P2，P3，P4，P5，P6）的多个计算机节点的分布式航空电子系统（100,500）。 分布式航空电子系统包括重新配置装置（332），该重新配置装置（332）被布置为在检测到至少一个计算机节点中的故障时重新配置分布式航空电子系统。 每个分区/应用程序都与应用程序/分区可用性级别相关联。 重新配置装置被配置为基于分区/应用（P1，P2，P3，P4，P5，P6）的分区/应用可用性级别来重新配置分布式航空电子系统。 本发明还涉及一种在具有多个计算机节点（A，B，C）的分布式航空电子系统中用于备份处理的方法。

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