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公开(公告)号：US09878805B2
公开(公告)日：2018-01-30
申请号：US14746046
申请日：2015-06-22
发明人： Stephen Judd , Nicholas Dallmann , Kevin McCabe , Daniel Seitz
摘要： A “black box” space vehicle solution may allow a payload developer to define the mission space and provide mission hardware within a predetermined volume and with predetermined connectivity. Components such as the power module, radios and boards, attitude determination and control system (ADCS), command and data handling (C&DH), etc. may all be provided as part of a “stock” (i.e., core) space vehicle. The payload provided by the payload developer may be plugged into the space vehicle payload section, tested, and launched without custom development of core space vehicle components by the payload developer. A docking station may facilitate convenient development and testing of the space vehicle while reducing handling thereof.
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公开(公告)号：US09760382B2
公开(公告)日：2017-09-12
申请号：US14745941
申请日：2015-06-22
发明人： Stephen Judd , Nicholas Dallmann , Kevin McCabe , Jerry Delapp , Dean Prichard , Michael Proicou , Daniel Seitz , Paul Stein , John Michel , Justin Tripp , Joseph Palmer , Steven Storms
CPC分类号： G06F9/44505 , G06F11/0739 , G06F11/0757 , G06F11/1417 , G06F11/1433
摘要： A space vehicle may have a modular board configuration that commonly uses some or all components and a common operating system for at least some of the boards. Each modular board may have its own dedicated processing, and processing loads may be distributed. The space vehicle may be reprogrammable, and may be launched without code that enables all functionality and/or components. Code errors may be detected and the space vehicle may be reset to a working code version to prevent system failure.
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公开(公告)号：US09478855B2
公开(公告)日：2016-10-25
申请号：US14745996
申请日：2015-06-22
发明人： Stephen Judd , Nicholas Dallmann , Jerry Delapp , Michael Proicou , Daniel Seitz , John Michel , Donald Enemark
CPC分类号： H04B7/1851 , H01Q3/02 , H04B7/155 , H04B7/185 , H04B7/18517
摘要： A field unit and ground station may use commercial off-the-shelf (COTS) components and share a common architecture, where differences in functionality are governed by software. The field units and ground stations may be easy to deploy, relatively inexpensive, and be relatively easy to operate. A novel file system may be used where datagrams of a file may be stored across multiple drives and/or devices. The datagrams may be received out of order and reassembled at the receiving device.
摘要翻译： 现场单元和地面站可以使用商业现成的（COTS）组件，并且共享共同的架构，其中功能的差异由软件控制。 现场单元和地面站可以容易地部署，相对便宜，并且相对容易操作。 可以使用一种新颖的文件系统，其中可以跨多个驱动器和/或设备存储文件的数据报。 数据报可能无法接收，并在接收设备重新组合。
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4.发明申请MODULAR SPACE VEHICLE BOARDS, CONTROL SOFTWARE, REPROGRAMMING, AND FAILURE RECOVERY 有权模块化空间车牌，控制软件，复制和故障恢复公开(公告)号：US20150370579A1
公开(公告)日：2015-12-24
申请号：US14745941
申请日：2015-06-22
发明人： Stephen Judd , Nicholas Dallmann , Kevin McCabe , Jerry Delapp , Dean Prichard , Michael Proicou , Daniel Seitz , Paul Stein , John Michel , Justin Tripp , Joseph Palmer , Steven Storms
CPC分类号： G06F9/44505 , G06F11/0739 , G06F11/0757 , G06F11/1417 , G06F11/1433
摘要： A space vehicle may have a modular board configuration that commonly uses some or all components and a common operating system for at least some of the boards. Each modular board may have its own dedicated processing, and processing loads may be distributed. The space vehicle may be reprogrammable, and may be launched without code that enables all functionality and/or components. Code errors may be detected and the space vehicle may be reset to a working code version to prevent system failure.
摘要翻译： 空间车辆可以具有通常使用一些或所有部件的模块化板配置和用于至少一些板的通用操作系统。 每个模块板可以具有其自己的专用处理，并且可以分配处理负载。 空间飞行器可以是可重新编程的，并且可以没有启用所有功能和/或组件的代码来启动。 可以检测到代码错误，并且空间车辆可以被重置为工作代码版本以防止系统故障。
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公开(公告)号：US10059468B1
公开(公告)日：2018-08-28
申请号：US15612534
申请日：2017-06-02
发明人： Stephen Judd , Nicholas Dallmann , Daniel Seitz , John Martinez , Steven Storms , Gayle Kestell
CPC分类号： B64G1/10 , B64G1/363 , B64G1/42 , B64G1/44 , B64G1/503 , B64G1/54 , B64G1/66 , B64G2001/1092
摘要： A modular space vehicle chassis may facilitate convenient access to internal components of the space vehicle. Each module may be removable from the others such that each module may be worked on individually. Multiple panels of at least one of the modules may swing open or otherwise be removable, exposing large portions of the internal components of the space vehicle. Such chassis architectures may reduce the time required for and difficulty of performing maintenance or modifications, may allow multiple space vehicles to take advantage of a common chassis design, and may further allow for highly customizable space vehicles.
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公开(公告)号：US09768857B1
公开(公告)日：2017-09-19
申请号：US15292384
申请日：2016-10-13
发明人： Stephen Judd , Nicholas Dallmann , Jerry Delapp , Michael Proicou , Daniel Seitz , John Michel , Donald Enemark
CPC分类号： H04B7/1851 , H01Q3/02 , H04B7/155 , H04B7/185 , H04B7/18517
摘要： A field unit and ground station may use commercial off-the-shelf (COTS) components and share a common architecture, where differences in functionality are governed by software. The field units and ground stations may be easy to deploy, relatively inexpensive, and be relatively easy to operate. A novel file system may be used where datagrams of a file may be stored across multiple drives and/or devices. The datagrams may be received out of order and reassembled at the receiving device.
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公开(公告)号：US09708080B2
公开(公告)日：2017-07-18
申请号：US14745698
申请日：2015-06-22
发明人： Stephen Judd , Nicholas Dallmann , Daniel Seitz , John Martinez , Steven Storms , Gayle Kestell
CPC分类号： B64G1/10 , B64G1/363 , B64G1/42 , B64G1/44 , B64G1/503 , B64G1/54 , B64G1/66 , B64G2001/1092
摘要： A modular space vehicle chassis may facilitate convenient access to internal components of the space vehicle. Each module may be removable from the others such that each module may be worked on individually. Multiple panels of at least one of the modules may swing open or otherwise be removable, exposing large portions of the internal components of the space vehicle. Such chassis architectures may reduce the time required for and difficulty of performing maintenance or modifications, may allow multiple space vehicles to take advantage of a common chassis design, and may further allow for highly customizable space vehicles.
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8.发明申请ATTITUDE DETERMINATION AND CONTROL SYSTEM (ADCS), SUN SENSOR, AND STAR TRACKER 审中-公开态度测定与控制系统（ADCS），太阳传感器和星踪仪公开(公告)号：US20150367966A1
公开(公告)日：2015-12-24
申请号：US14745875
申请日：2015-06-22
发明人： Stephen Judd , Nicholas Dallmann , Michael Proicou , Daniel Seitz , Paul Stein , John Martinez , Gayle Kestell , Adam Warniment , Steven Storms
摘要： An ADCS module may be configured to use coordinate data from 2D photodiodes in one or more sun sensors to determine a sun vector. The ADCS module may then use the sun vector in reference to its own body faced (BF) coordinate system to calculate a change in the orientation of the space vehicle. The change in orientation mechanism may be accomplished by reaction wheels, ion thrusters, or other orientation altering mechanisms. A miniature, intelligent star tracker may be included that improves satellite attitude determination and pointing accuracy. An improved reaction wheel assembly may be included that is more robust and suitable for inclusion in small space vehicles.
摘要翻译： ADCS模块可以被配置为在一个或多个太阳传感器中使用来自2D光电二极管的坐标数据来确定太阳矢量。 然后，ADCS模块可以参考其自身的身体（BF）坐标系来使用太阳矢量来计算空间车辆的取向的变化。 取向机构的变化可以通过反作用轮，离子推进器或其它取向改变机构来实现。 可以包括一种微型智能星形跟踪器，可以改善卫星姿态确定和指向精度。 可以包括改进的反作用轮组件，其更加坚固并且适合于包含在小型空间车辆中。
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公开(公告)号：US20150367965A1
公开(公告)日：2015-12-24
申请号：US14746046
申请日：2015-06-22
发明人： Stephen Judd , Nicholas Dallmann , Kevin McCabe , Daniel Seitz
IPC分类号： B64G1/22
摘要： A “black box” space vehicle solution may allow a payload developer to define the mission space and provide mission hardware within a predetermined volume and with predetermined connectivity. Components such as the power module, radios and boards, attitude determination and control system (ADCS), command and data handling (C&DH), etc. may all be provided as part of a “stock” (i.e., core) space vehicle. The payload provided by the payload developer may be plugged into the space vehicle payload section, tested, and launched without custom development of core space vehicle components by the payload developer. A docking station may facilitate convenient development and testing of the space vehicle while reducing handling thereof.
摘要翻译： “黑匣子”空间车辆解决方案可以允许有效载荷开发者定义任务空间并且在预定的体积内并具有预定的连接性来提供任务硬件。 诸如电源模块，无线电和电路板，姿态确定和控制系统（ADCS），命令和数据处理（C＆DH）等组件都可以作为“库存”（即核心）空间车辆的一部分提供。 由有效载荷开发者提供的有效载荷可以被插入到空间载荷有效载荷部分中，被测试和启动，而无需有效载荷开发者定制开发核心空间车辆部件。 对接站可以促进对空间车辆的便利开发和测试，同时减少其处理。
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公开(公告)号：US20150372380A1
公开(公告)日：2015-12-24
申请号：US14745996
申请日：2015-06-22
发明人： Stephen Judd , Nicholas Dallmann , Jerry Delapp , Michael Proicou , Daniel Seitz , John Michel , Donald Enemark
CPC分类号： H04B7/1851 , H01Q3/02 , H04B7/155 , H04B7/185 , H04B7/18517
摘要： A field unit and ground station may use commercial off-the-shelf (COTS) components and share a common architecture, where differences in functionality are governed by software. The field units and ground stations may be easy to deploy, relatively inexpensive, and be relatively easy to operate. A novel file system may be used where datagrams of a file may be stored across multiple drives and/or devices. The datagrams may be received out of order and reassembled at the receiving device.
摘要翻译： 现场单元和地面站可以使用商业现成的（COTS）组件，并且共享共同的架构，其中功能的差异由软件控制。 现场单元和地面站可以容易地部署，相对便宜，并且相对容易操作。 可以使用一种新颖的文件系统，其中可以跨多个驱动器和/或设备存储文件的数据报。 数据报可能无法接收，并在接收设备重新组合。
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