Configurable space station momentum
    2.
    发明授权
    Configurable space station momentum 有权
    可配置的空间站动量

    公开(公告)号:US09511882B2

    公开(公告)日:2016-12-06

    申请号:US14280132

    申请日:2014-05-16

    Abstract: A method of deploying a modular space station comprises placing an initial space station module in space in a first deployment, the initial space station module including a first control law and momentum component that provides an initial solution for guidance, navigation, and control (GNC) during the first deployment. A first space station modular segment is joined with the initial space station module in a second deployment to produce a first joint configuration of the space station. A second control law and momentum component provides a second solution for GNC of the first joint configuration during the second deployment. A second space station modular segment is joined to the first joint configuration in a third deployment to produce a second joint configuration of the space station. A third control law and momentum component provides a third solution for GNC of the second joint configuration during the third deployment.

    Abstract translation: 一种部署模块化空间站的方法包括将初始空间站模块放置在第一次部署中的空间中,初始空间站模块包括第一控制定律和动量分量,其为引导,导航和控制(GNC)提供初始解决方案, 在第一次部署期间。 在第二部署中,第一空间站模块段与初始空间站模块相连,以产生空间站的第一联合配置。 第二个控制规则和动量组件为第二次部署期间第一个联合配置的GNC提供了第二个解决方案。 在第三部署中第二空间站模块化段连接到第一联合配置以产生空间站的第二联合配置。 第三个控制规律和动量组件为第三次部署期间的第二个联合配置的GNC提供了第三个解决方案。

    COMPACT PROXIMITY DISPLAY UTILIZING IMAGE TRANSFER
    3.
    发明申请
    COMPACT PROXIMITY DISPLAY UTILIZING IMAGE TRANSFER 有权
    使用图像传输的紧凑近似显示

    公开(公告)号:US20160131906A1

    公开(公告)日:2016-05-12

    申请号:US14535968

    申请日:2014-11-07

    CPC classification number: G02B27/0172 G02B6/06 G02B27/017

    Abstract: A compact proximity display system and method that employs an image transfer device is provided. The system and method employs an image transfer device, such as a fiber optic device, which enables remotely locating an image generating source from the display assembly that is mounted on, or proximate to, the helmet bubble, thereby reducing the amount of components located proximate to the helmet bubble. The system and method minimize the intrusion of the entire display system into user's viewing area, and increase safety.

    Abstract translation: 提供采用图像传送装置的紧凑型接近显示系统和方法。 该系统和方法采用诸如光纤设备的图像传送装置,其能够从安装在头盔气泡上或附近的显示组件远程定位图像生成源,从而减少位于最近的部件的量 到头盔泡沫。 系统和方法将整个显示系统的入侵最小化到用户的观看区域,并增加安全性。

    CONSOLIDATED VEHICLE PROPULSION CONTROL USING INTEGRATED MODULAR AVIONICS
    4.
    发明申请
    CONSOLIDATED VEHICLE PROPULSION CONTROL USING INTEGRATED MODULAR AVIONICS 有权
    使用综合模块化航空的综合车辆推进控制

    公开(公告)号:US20140121862A1

    公开(公告)日:2014-05-01

    申请号:US13666565

    申请日:2012-11-01

    CPC classification number: B64C19/00 B64G1/00

    Abstract: A vehicle is provided. The vehicle may include, but is not limited to, a virtual backplane, a vehicle management computer communicatively coupled to the first virtual backplane and having a first predetermined schedule, a consolidated propulsion controller communicatively coupled to the virtual backplane and having a second predetermined schedule different from the first predetermined schedule, at least one engine communicatively coupled to the first virtual backplane, each of the at least one engines having a unique schedule, and at least one control system communicatively coupled to the first virtual backplane, each of the at least one control systems having a unique schedule, wherein each of the vehicle management computer, consolidated propulsion controller, at least one engines and at least one control system are configured to add and consume date from the virtual backplane according to their respective schedules.

    Abstract translation: 提供车辆。 车辆可以包括但不限于虚拟背板,通信地耦合到第一虚拟背板并具有第一预定时间表的车辆管理计算机,通信地耦合到虚拟背板并具有第二预定时间表的综合推进控制器 从所述第一预定时间表,至少一个通信地耦合到所述第一虚拟背板的引擎,所述至少一个引擎中的每一个具有唯一的调度,以及至少一个通信地耦合到所述第一虚拟背板的控制系统,所述至少一个 控制系统具有独特的时间表,其中,车辆管理计算机,综合推进控制器,至少一个引擎和至少一个控制系统中的每一个被配置为根据它们各自的时间表从虚拟背板增加和消耗日期。

    INTEGRATED AVIONICS SYSTEMS AND METHODS
    5.
    发明申请
    INTEGRATED AVIONICS SYSTEMS AND METHODS 有权
    综合航空系统与方法

    公开(公告)号:US20140301384A1

    公开(公告)日:2014-10-09

    申请号:US13857890

    申请日:2013-04-05

    CPC classification number: H04W56/001 H04B7/18506

    Abstract: Systems and methods are described for synchronizing data in a mobile platform. In one embodiment, a method for synchronizing data in a mobile platform is provided. The method includes: receiving a first synchronization signal at a first remote interface unit from a signal generator; receiving a second synchronization signal at a second remote interface unit from the signal generator; and executing a synchronization state machine of the first and second remote interface units based on the first and second synchronization signals to synchronize outputs of the first and second remote interface units.

    Abstract translation: 描述了用于在移动平台中同步数据的系统和方法。 在一个实施例中,提供了一种用于在移动平台中同步数据的方法。 该方法包括:在第一远程接口单元处从信号发生器接收第一同步信号; 在信号发生器的第二远程接口单元处接收第二同步信号; 以及基于所述第一和第二同步信号执行所述第一和第二远程接口单元的同步状态机,以同步所述第一和第二远程接口单元的输出。

    Integrated avionics systems and methods

    公开(公告)号:US09706508B2

    公开(公告)日:2017-07-11

    申请号:US13857890

    申请日:2013-04-05

    CPC classification number: H04W56/001 H04B7/18506

    Abstract: Systems and methods are described for synchronizing data in a mobile platform. In one embodiment, a method for synchronizing data in a mobile platform is provided. The method includes: receiving a first synchronization signal at a first remote interface unit from a signal generator; receiving a second synchronization signal at a second remote interface unit from the signal generator; and executing a synchronization state machine of the first and second remote interface units based on the first and second synchronization signals to synchronize outputs of the first and second remote interface units.

    SYSTEMS AND METHODS FOR A MOMENTUM PLATFORM
    7.
    发明申请
    SYSTEMS AND METHODS FOR A MOMENTUM PLATFORM 审中-公开
    一个动物平台的系统和方法

    公开(公告)号:US20150367968A1

    公开(公告)日:2015-12-24

    申请号:US14309275

    申请日:2014-06-19

    CPC classification number: B64G4/00 B64G1/244 B64G1/283 B64G1/286 B64G6/00

    Abstract: Systems and methods for a momentum platform are provided. For example, a system for opposing torques includes a platform, wherein the platform is transportable to different locations in a zero-gravity environment and a plurality of momentum devices within the platform, wherein the plurality of momentum devices provide controllable angular momentum. The system also includes a torque feedback device, wherein the torque feedback device detects the torques experienced by the platform; a processing unit that controls the angular momentum of the plurality of momentum devices based on the torques detected by the torque feedback device such that the platform remains stable in response to the torques; and a mounting surface on the platform for attaching objects to the platform.

    Abstract translation: 提供了动量平台的系统和方法。 例如,用于相反扭矩的系统包括平台,其中平台可运输到零重力环境中的不同位置和平台内的多个动量装置,其中多个动量装置提供可控角动量。 该系统还包括扭矩反馈装置,其中扭矩反馈装置检测平台经历的转矩; 处理单元,其基于由所述扭矩反馈装置检测的扭矩来控制所述多个动量装置的角动量,使得所述平台响应于所述转矩而保持稳定; 以及用于将物体附接到平台的平台上的安装表面。

    CONFIGURABLE SPACE STATION MOMENTUM
    8.
    发明申请
    CONFIGURABLE SPACE STATION MOMENTUM 有权
    可配置空间站动画

    公开(公告)号:US20150329222A1

    公开(公告)日:2015-11-19

    申请号:US14280132

    申请日:2014-05-16

    Abstract: A method of deploying a modular space station comprises placing an initial space station module in space in a first deployment, the initial space station module including a first control law and momentum component that provides an initial solution for guidance, navigation, and control (GNC) during the first deployment. A first space station modular segment is joined with the initial space station module in a second deployment to produce a first joint configuration of the space station. A second control law and momentum component provides a second solution for GNC of the first joint configuration during the second deployment. A second space station modular segment is joined to the first joint configuration in a third deployment to produce a second joint configuration of the space station. A third control law and momentum component provides a third solution for GNC of the second joint configuration during the third deployment.

    Abstract translation: 一种部署模块化空间站的方法包括将初始空间站模块放置在第一次部署中的空间中,初始空间站模块包括第一控制定律和动量分量,其为引导,导航和控制(GNC)提供初始解决方案, 在第一次部署期间。 在第二部署中,第一空间站模块段与初始空间站模块相连,以产生空间站的第一联合配置。 第二个控制规则和动量组件为第二次部署期间第一个联合配置的GNC提供了第二个解决方案。 在第三部署中第二空间站模块化段连接到第一联合配置以产生空间站的第二联合配置。 第三个控制规律和动量组件为第三次部署期间的第二个联合配置的GNC提供了第三个解决方案。

    Consolidated vehicle propulsion control using integrated modular avionics
    9.
    发明授权
    Consolidated vehicle propulsion control using integrated modular avionics 有权
    综合车辆推进控制采用集成模块化航空电子设备

    公开(公告)号:US08868260B2

    公开(公告)日:2014-10-21

    申请号:US13666565

    申请日:2012-11-01

    CPC classification number: B64C19/00 B64G1/00

    Abstract: A vehicle is provided. The vehicle may include, but is not limited to, a virtual backplane, a vehicle management computer communicatively coupled to the first virtual backplane and having a first predetermined schedule, a consolidated propulsion controller communicatively coupled to the virtual backplane and having a second predetermined schedule different from the first predetermined schedule, at least one engine communicatively coupled to the first virtual backplane, each of the at least one engines having a unique schedule, and at least one control system communicatively coupled to the first virtual backplane, each of the at least one control systems having a unique schedule, wherein each of the vehicle management computer, consolidated propulsion controller, at least one engines and at least one control system are configured to add and consume date from the virtual backplane according to their respective schedules.

    Abstract translation: 提供车辆。 车辆可以包括但不限于虚拟背板,通信地耦合到第一虚拟背板并具有第一预定时间表的车辆管理计算机,通信地耦合到虚拟背板并具有第二预定时间表的综合推进控制器 从所述第一预定时间表,至少一个通信地耦合到所述第一虚拟背板的引擎,所述至少一个引擎中的每一个具有唯一的调度,以及至少一个通信地耦合到所述第一虚拟背板的控制系统,所述至少一个 控制系统具有独特的时间表,其中,车辆管理计算机,综合推进控制器,至少一个引擎和至少一个控制系统中的每一个被配置为根据它们各自的时间表从虚拟背板增加和消耗日期。

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