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    • 3. 发明申请
    • ETHERNET FOR AVIONICS
    • 以太网的航空
    • US20130170498A1
    • 2013-07-04
    • US13704863
    • 2010-06-17
    • Torkel DanielssonAnders PetterssonAnders GripsbornJan Håkegård
    • Torkel DanielssonAnders PetterssonAnders GripsbornJan Håkegård
    • H04L12/56
    • H04L47/826H04L12/4015H04L2012/4028
    • An avionics switched Ethernet network. A plurality of synchronized interconnected system nodes each includes an avionics module arranged to periodically provide a set of data messages. Each message includes a set of data variables. A network module couples the avionics module to the network. The network module includes a network interface unit arranged to provide for transmission of data packets including a number of the data messages from the avionics module. The network module of each system node includes a transmission control unit arranged to control the network interface unit to perform scheduled transmissions of the data packets. The transmission control unit is provided with access to a memory module. Each of the plurality of time-slots is statically allocated a predetermined number of data packets, each including a predetermined subset of data messages from the set of data messages.
    • 航空电子交换以太网。 多个同步的互连系统节点每个包括布置成周期性地提供一组数据消息的航空电子模块。 每条消息都包含一组数据变量。 网络模块将航空电子模块耦合到网络。 网络模块包括网络接口单元,网络接口单元被布置成提供包括来自航空电子模块的多个数据消息的数据分组的传输。 每个系统节点的网络模块包括传输控制单元,其被布置为控制网络接口单元执行数据分组的调度传输。 传输控制单元被提供到存储器模块的访问。 多个时隙中的每一个被静态地分配预定数量的数据分组,每个数据分组包括来自该组数据消息的数据消息的预定子集。
    • 4. 发明申请
    • DISTRIBUTED AVIONICS SYSTEM AND METHOD FOR BACKUP HANDLING IN AN AVIONICS SYSTEM
    • 分布式AVIONICS系统和方法在海洋系统中的备份处理
    • US20140157041A1
    • 2014-06-05
    • US14113554
    • 2011-05-17
    • Torkel DanielssonJan HåkegårdAnders Gripsborn
    • Torkel DanielssonJan HåkegårdAnders Gripsborn
    • G06F11/20
    • G06F11/2041G06F11/143G06F11/203G06F11/2035G06F11/2043
    • 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).
    • 本发明涉及一种分布式航空电子系统(100,500),其具有被布置为执行多个分区/应用(P1,P2,P3,P4,P5,P6)的多个计算机节点。 分布式航空电子系统包括重新配置装置(332),其被配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/应用程序与应用程序/分区可用性级别相关联。 重新配置装置被布置为基于分区/应用(P1,P2,P3,P4,P5,P6)的分区/应用可用性级别重新配置分布式航空电子系统。 本发明还涉及具有多个计算机节点(A,B,C)的分布式航空电子系统中的后备处理方法。
    • 6. 发明申请
    • CONFIGURABLE INPUT/OUTPUT PROCESSOR
    • 可配置输入/输出处理器
    • US20140089534A1
    • 2014-03-27
    • US14115763
    • 2011-05-06
    • Jan HåkegårdTorkel DanielssonAnders Gripsborn
    • Jan HåkegårdTorkel DanielssonAnders Gripsborn
    • G06F3/00
    • G06F3/002H04L67/12H04W4/70
    • 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.
    • 本发明涉及可配置的输入/输出处理设备,用于配置可配置输入/输出处理设备的方法和用于执行该方法的步骤的计算机程序产品。 可配置输入/输出处理设备(6)被布置为控制与包括在网络(2)中互连的多个处理节点的分布式航空电子设备控制系统相关联的数据流量,其中多个处理节点中的每一个连接到网络 经由所述可配置输入/输出处理装置中的至少一个。 可配置输入/输出处理器包括第一指令(CCR),所述第一指令包括用于至少一个输入/输出处理设备的处理信息,并且独立于分布式航空电子设备控制系统和第二指令(SCT)的当前配置,所述 第二指令取决于分布式航空电子设备控制系统的当前配置。
    • 7. 发明授权
    • Distributed avionics
    • 分布式航空电子设备
    • US08543263B2
    • 2013-09-24
    • US13704890
    • 2010-06-17
    • Torkel DanielssonAnders PetterssonJan Håkegård
    • Torkel DanielssonAnders PetterssonJan Håkegård
    • G01C23/00
    • G06F17/00G06F9/4887H04L67/12H04L67/322H04L69/28
    • A distributed avionics system arranged in an aerial vehicle for controlling at least one avionics function. A plurality of avionics processing subsystems are interconnected in a network. Each avionics processing subsystem includes a processor arranged to process at least one task so as to provide a set of data messages including at least one unit of data related to controlling the at least one avionics function on basis of provided input data, related to conditions of the at least one avionics function. A memory module is in operative connection with the processor and is arranged to store instructions for the processor to process the at least one task. At least one of the avionics processing subsystems is arranged to transmit at least one synchronization cycle start signal onto the network.
    • 一种布置在飞行器中用于控制至少一个航空电子系统功能的分布式航空电子系统。 多个航空电子处理子系统在网络中互连。 每个航空电子处理子系统包括处理器,其被布置为处理至少一个任务,以便提供一组数据消息,包括与所提供的输入数据有关的至少一个与控制所述至少一个航空电子系统功能相关的数据单元, 至少一个航空电子系统功能。 存储器模块与处理器操作连接,并且被布置为存储处理器处理该至少一个任务的指令。 航空电子学处理子系统中的至少一个被布置成将至少一个同步周期开始信号发送到网络上。
    • 8. 发明申请
    • DISTRIBUTED AVIONICS
    • 分布式航空
    • US20130138271A1
    • 2013-05-30
    • US13704890
    • 2010-06-17
    • Torkel DanielssonAnders PetterssonJan Håkegård
    • Torkel DanielssonAnders PetterssonJan Håkegård
    • G06F17/00
    • G06F17/00G06F9/4887H04L67/12H04L67/322H04L69/28
    • A distributed avionics system arranged in an aerial vehicle for controlling at least one avionics function. A plurality of avionics processing subsystems are interconnected in a network. Each avionics processing subsystem includes a processor arranged to process at least one task so as to provide a set of data messages including at least one unit of data related to controlling the at least one avionics function on basis of provided input data, related to conditions of the at least one avionics function. A memory module is in operative connection with the processor and is arranged to store instructions for the processor to process the at least one task. At least one of the avionics processing subsystems is arranged to transmit at least one synchronization cycle start signal onto the network
    • 一种布置在飞行器中用于控制至少一个航空电子系统功能的分布式航空电子系统。 多个航空电子处理子系统在网络中互连。 每个航空电子处理子系统包括处理器,其被布置为处理至少一个任务,以便提供一组数据消息,包括与所提供的输入数据有关的至少一个与控制所述至少一个航空电子系统功能相关的数据单元, 至少一个航空电子系统功能。 存储器模块与处理器操作连接,并且被布置为存储处理器处理该至少一个任务的指令。 航空电子学处理子系统中的至少一个被布置成将至少一个同步周期开始信号发送到网络上
    • 9. 发明申请
    • VEHICULAR DISPLAY SYSTEM AND A METHOD FOR CONTROLLING THE DISPLAY SYSTEM
    • 车辆显示系统和控制显示系统的方法
    • US20130038525A1
    • 2013-02-14
    • US13578661
    • 2010-02-12
    • Jan HåkegårdAnders PetterssonTorkel Danielsson
    • Jan HåkegårdAnders PetterssonTorkel Danielsson
    • G06F3/038G06F3/01
    • G01C23/00G06F3/1438G06F3/147G09G2380/12
    • A vehicular control system including a plurality of displays each including a physical display unit and memory module including information related to descriptions of a plurality of displayable entities and first configuration data, associated to a first control module. The first configuration data including information on configuration of the displayable entities, based on references to the descriptions of the plurality of displayable entities. The memory module of each display comprises a copy of the first configuration data. The first control module is arranged to transmit data based on point-to-multipoint communication to each of the plurality of displays. The plurality of displays each includes a processor operatively coupled to the memory module. The processor is arranged to process the entities based on received data from the first control module and to present the result of the processing on the physical display unit of each of the displays.
    • 一种包括多个显示器的车辆控制系统,每个显示器包括与第一控制模块相关联的物理显示单元和包括与多个可显示实体和第一配置数据的描述有关的信息的存储器模块。 基于对多个可显示实体的描述的引用,第一配置数据包括关于可显示实体的配置的信息。 每个显示器的存储器模块包括第一配置数据的副本。 第一控制模块被布置为基于点对多点通信向多个显示器中的每一个发送数据。 多个显示器包括可操作地耦合到存储器模块的处理器。 处理器被布置为基于来自第一控制模块的接收数据处理实体,并且在每个显示器的物理显示单元上呈现处理结果。
    • 10. 发明申请
    • SIMULATING AND TESTING AVIONICS
    • 模拟和测试电影
    • US20130166271A1
    • 2013-06-27
    • US13808839
    • 2010-07-06
    • Torkel DanielssonAnders Pettersson
    • Torkel DanielssonAnders Pettersson
    • G06F17/50
    • G06F17/5009G06F9/44505G06F11/3664G06F11/3668
    • An avionics application host system and method for simulating and/or testing a plurality of partitioned applications arranged to be periodically executed on a target system. The target system is a distributed avionics control system of an aerial vehicle. The host system includes a plurality of functional modules. The plurality of functional modules includes: an application module arranged to import the plurality of partitioned applications in un-modified form, a configuration module arranged to configure the operations of the host system, at least one communication module arranged to provide communication between the partitioned applications, a control module arranged to provide coordinated execution time to the functional modules, a service module associated to each imported partitioned application arranged to provide services to the imported partitioned applications so as to enable execution of the imported partitioned applications and to preserve the temporal order of events related to communication and execution.
    • 一种用于模拟和/或测试被布置为在目标系统上周期性执行的多个分区应用的航空电子应用主机系统和方法。 目标系统是飞行器的分布式航空电子控制系统。 主机系统包括多个功能模块。 多个功能模块包括:应用模块,其布置成以未修改的形式导入多个分割的应用;配置模块,被布置成配置主机系统的操作;至少一个通信模块,被布置为提供分区应用之间的通信 控制模块,其被布置为向所述功能模块提供协调的执行时间;与每个导入的分区应用相关联的服务模块,被布置为向所述导入的分区应用程序提供服务,以便能够执行所述导入的分区应用程序,并且保持时间顺序 与沟通和执行相关的事件。