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1. 发明申请

US20050105772A1 Optical body tracker 审中-公开
标题翻译：光学身体追踪器
公开(公告)号：US20050105772A1
公开(公告)日：2005-05-19
申请号：US10958457
申请日：2004-10-05
申请人： Nestor Voronka , Charles Jacobus
发明人： Nestor Voronka , Charles Jacobus
IPC分类号： G06F3/00 , G06F3/01 , G06K9/00 , G06T7/20
CPC分类号： G06F3/017 , A61B5/1127 , A63F2300/1087 , G06K9/00335 , G06T7/246
摘要： An optical system tracks the motion of objects, including the human body or portions thereof using a plurality of three-dimensional active markers based upon triangulation from data read via multiple linear CCDs through cylindrical lenses. Each marker is lit in sequence so that it is in sync with a frame capture using the imaging system positioned and oriented so as to provide a basis for computing three-dimensional location. In the preferred embodiment, the imaging system detects an infrared signal which is sent out by the tag controller as part of the tag/marker illumination sequence at the beginning of the first tag position capture time. The controller then traverses through the tags in time sync with each imaging system frame capture cycle. Thus, only one unique tag will be lit during each image capture of the cameras, thereby simplifying identification. Using linear CCD sensors, the frame time (i.e. point acquisition time) is very short, allowing very many markers to be sampled and located sequentially in real time.
摘要翻译：光学系统基于通过多个线性CCD通过柱面透镜读取的数据的三角测量，使用多个三维有源标记跟踪物体的运动，包括人体或其部分。每个标记物依次点亮，使得它与使用定位和定向的成像系统的帧捕获同步，以便为计算三维位置提供基础。在优选实施例中，成像系统在第一标签位置捕获时间的开始处检测作为标签/标记照明序列的一部分由标签控制器发送的红外信号。然后，控制器在与每个成像系统帧捕获周期的时间同步中遍历标签。因此，在摄像机的每次图像拍摄期间，仅一个唯一标签将被点亮，从而简化了识别。使用线性CCD传感器，帧时间（即点采集时间）非常短，允许非常多的标记被实时采样和定位。

2. 发明申请

US20050127243A1 Automatic reserve or primary parachute activation device 失效
标题翻译：自动储备或主降落伞激活装置
公开(公告)号：US20050127243A1
公开(公告)日：2005-06-16
申请号：US10972703
申请日：2004-10-25
申请人： Nestor Voronka , Charles Jacobus , Derek Johnson , Pavan Namineni
发明人： Nestor Voronka , Charles Jacobus , Derek Johnson , Pavan Namineni
IPC分类号： B64D17/56 , B64D17/58
CPC分类号： B64D17/56
摘要： An electronic automatic reserve or primary parachute activation device incorporates partial or complete capture of freefaller or tethered parachute jumper kinematics to rapidly and reliable determine when to automatically activate deployment of the primary or reserve chute. This device uses means for directly measuring acceleration, velocity and/or position in addition to air pressure change to enable reliable detection of chute deployment conditions earlier than is possible with conventional pressure change activated automated activations devices. This is important when the activation decision must be made within 5-10 seconds of the initiation of the jump as is the case for military low altitude parachuting.
摘要翻译：电子自动储备或主降落伞激活装置包括部分或完全捕获自由落体或拴系降落伞跳跃运动学，以快速可靠地确定何时自动激活主滑槽或预留滑槽的部署。该装置除了气压变化之外还使用直接测量加速度，速度和/或位置的装置，以使得能够比常规压力变化激活的自动激活装置更早地可靠地检测滑槽部署状况。当激活决定必须在启动跳跃的5-10秒内进行激活，这与军事低空跳伞的情况一样重要。

3. 发明授权

US07073752B2 Automatic reserve or primary parachute activation device 失效
标题翻译：自动储备或主降落伞激活装置
公开(公告)号：US07073752B2
公开(公告)日：2006-07-11
申请号：US10972703
申请日：2004-10-25
申请人： Nestor Voronka , Charles J. Jacobus , Derek M. Johnson , Pavan Namineni
发明人： Nestor Voronka , Charles J. Jacobus , Derek M. Johnson , Pavan Namineni
IPC分类号： B64D17/54
CPC分类号： B64D17/56
摘要： An electronic automatic reserve or primary parachute activation device incorporates partial or complete capture of freefaller or tethered parachute jumper kinematics to rapidly and reliable determine when to automatically activate deployment of the primary or reserve chute. This device uses means for directly measuring acceleration, velocity and/or position in addition to air pressure change to enable reliable detection of chute deployment conditions earlier than is possible with conventional pressure change activated automated activations devices. This is important when the activation decision must be made within 5–10 seconds of the initiation of the jump as is the case for military low altitude parachuting.
摘要翻译：电子自动储备或主降落伞激活装置包括部分或完全捕获自由落体或拴系降落伞跳跃运动学，以快速可靠地确定何时自动激活主滑槽或预留滑槽的部署。该装置除了气压变化之外还使用直接测量加速度，速度和/或位置的装置，以使得能够比常规压力变化激活的自动激活装置更早地可靠地检测滑槽部署状况。当激活决定必须在启动跳跃的5-10秒内进行激活，这与军事低空跳伞的情况一样重要。

4. 发明申请

US20170239723A1 Structures with Internal Microstructures to Provide Multifunctional Capabilities 审中-公开
公开(公告)号：US20170239723A1
公开(公告)日：2017-08-24
申请号：US15452727
申请日：2017-03-07
申请人： Robert Hoyt , Jonathan Wrobel , Jesse Cushing , Mark Jaster , Nestor Voronka , Scott Frank , Jeffrey Slostad , Leonid Paritsky
发明人： Robert Hoyt , Jonathan Wrobel , Jesse Cushing , Mark Jaster , Nestor Voronka , Scott Frank , Jeffrey Slostad , Leonid Paritsky
IPC分类号： B22F3/105 , B64G1/58 , B29C67/00 , G21F1/12 , B33Y80/00 , B22F7/00 , B22F7/02 , B23K15/00 , B64G1/54 , B33Y10/00
CPC分类号： B22F3/1055 , B22F7/008 , B22F7/02 , B22F2302/45 , B22F2998/10 , B23K15/0086 , B23K2103/172 , B23K2103/18 , B23K2103/42 , B29C64/106 , B29C64/112 , B29C64/153 , B29L2031/3002 , B29L2031/3097 , B33Y10/00 , B33Y80/00 , B64G1/506 , B64G1/54 , B64G1/58 , G21F1/12 , Y02P10/295
摘要： A structural spacecraft component comprising internal microstructure; wherein said microstructure comprises a plurality of parallel layers and a plurality of spacers that connect adjacent parallel layers; wherein said structural spacecraft component is a product of an additive manufacturing process.

5. 发明申请

US20150048209A1 Structures with Internal Microstructures to Provide Multifunctional Capabilities 审中-公开
标题翻译：具有内部微结构以提供多功能能力的结构
公开(公告)号：US20150048209A1
公开(公告)日：2015-02-19
申请号：US14462541
申请日：2014-08-18
申请人： Robert Hoyt , Jonathan Wrobel , Jesse Cushing , Mark Jaster , Nestor Voronka , Scott Frank , Jeffrey Slostad , Leonid Paritsky
发明人： Robert Hoyt , Jonathan Wrobel , Jesse Cushing , Mark Jaster , Nestor Voronka , Scott Frank , Jeffrey Slostad , Leonid Paritsky
IPC分类号： B64G1/54 , B22F7/02 , B22F3/105 , B64G1/22 , B29C67/00
CPC分类号： B22F3/1055 , B22F7/008 , B22F7/02 , B22F2302/45 , B22F2998/10 , B23K15/0086 , B23K2103/172 , B23K2103/18 , B23K2103/42 , B29C64/106 , B29C64/112 , B29C64/153 , B29L2031/3002 , B29L2031/3097 , B33Y10/00 , B33Y80/00 , B64G1/506 , B64G1/54 , B64G1/58 , G21F1/12 , Y02P10/295
摘要： A structural spacecraft component comprising internal microstructure; wherein said microstructure comprises a plurality of parallel layers and a plurality of spacers that connect adjacent parallel layers; wherein said structural spacecraft component is a product of an additive manufacturing process.
摘要翻译：包括内部微结构的结构航天器部件; 其中所述微结构包括多个平行层和连接相邻平行层的多个间隔物; 其中所述结构航天器部件是添加剂制造过程的产物。

6. 发明申请

US20120138748A1 TERMINATOR TAPE SATELLITE DEORBIT MODULE 有权
标题翻译：终端带卫星定位模块
公开(公告)号：US20120138748A1
公开(公告)日：2012-06-07
申请号：US13318330
申请日：2010-04-30
申请人： Ian M. Barnes , Nestor Voronka , Robert Hoyt , Jeffrey Thor Slostad
发明人： Ian M. Barnes , Nestor Voronka , Robert Hoyt , Jeffrey Thor Slostad
IPC分类号： B64G1/22 , B64G1/10
CPC分类号： B64G1/007 , B64G1/242 , B64G1/62 , B64G1/648
摘要： A deorbit device comprising a passive electrodynamic conductive tape connected at one end to a spacecraft.
摘要翻译：一种包括在一端连接到航天器的无源电动导电带的脱轨装置。

7. 发明授权

US09016635B2 Terminator tape satellite deorbit module 有权
标题翻译：终结者磁带卫星雷达模块
公开(公告)号：US09016635B2
公开(公告)日：2015-04-28
申请号：US13318330
申请日：2010-04-30
申请人： Robert Hoyt , Ian Barnes , Nestor Voronka , Jeffrey Thor Slostad
发明人： Robert Hoyt , Ian Barnes , Nestor Voronka , Jeffrey Thor Slostad
IPC分类号： B64G1/00 , B64G1/34 , B64G1/62 , B64G1/24 , B64G1/64
CPC分类号： B64G1/007 , B64G1/242 , B64G1/62 , B64G1/648
摘要： A deorbit device comprising a passive electrodynamic conductive tape connected at one end to a spacecraft.
摘要翻译：一种包括在一端连接到航天器的无源电动导电带的脱轨装置。

8. 发明授权

US06801637B2 Optical body tracker 有权
标题翻译：光学身体追踪器
公开(公告)号：US06801637B2
公开(公告)日：2004-10-05
申请号：US09791123
申请日：2001-02-22
申请人： Nestor Voronka , Charles J. Jacobus
发明人： Nestor Voronka , Charles J. Jacobus
IPC分类号： G06K900
CPC分类号： G06K9/00335 , A63F2300/1087 , G06T7/246
摘要： An optical system tracks the motion of objects, including the human body or portions thereof using a plurality of three-dimensional active markers based upon triangulation from data read via multiple linear CCDs through cylindrical lenses. Each marker is lit in sequence so that it is in sync with a frame capture using the imaging system positioned and oriented so as to provide a basis for computing three-dimensional location. In the preferred embodiment, the imaging system detects an infrared signal which is sent out by the tag controller as part of the tag/marker illumination sequence at the beginning of the first tag position capture time. The controller then traverses through the tags in time sync with each imaging system frame capture cycle. Thus, only one unique tag will be lit during each image capture of the cameras, thereby simplifying identification. Using linear CCD sensors, the frame time (i.e. point acquisition time) is very short, allowing very many markers to be sampled and located sequentially in real time.
摘要翻译：光学系统基于通过多个线性CCD通过柱面透镜读取的数据的三角测量，使用多个三维有源标记跟踪物体的运动，包括人体或其部分。每个标记物依次点亮，使得它与使用定位和定向的成像系统的帧捕获同步，以便为计算三维位置提供基础。在优选实施例中，成像系统在第一标签位置捕获时间的开始处检测作为标签/标记照明序列的一部分由标签控制器发送的红外信号。然后，控制器在与每个成像系统帧捕获周期的时间同步中遍历标签。因此，在摄像机的每次图像拍摄期间，仅一个唯一标签将被点亮，从而简化了识别。使用线性CCD传感器，帧时间（即点采集时间）非常短，允许非常多的标记被实时采样和定位。

9. 发明授权

US06299308B1 Low-cost non-imaging eye tracker system for computer control 有权
标题翻译：用于计算机控制的低成本非成像眼动仪系统
公开(公告)号：US06299308B1
公开(公告)日：2001-10-09
申请号：US09540314
申请日：2000-03-31
申请人： Nestor Voronka , Charles J. Jacobus
发明人： Nestor Voronka , Charles J. Jacobus
IPC分类号： A61B314
CPC分类号： G06F3/013 , G02B27/017
摘要： A device for measuring eye movements is suitable for stand-alone, portable use and for integration into a head/helmet mounted display. The low-cost non-imaging eye tracking system is optimized toward the applications requiring computer cursor control by localizing the gaze direction as an operator looks through a fixed frame to provide pointing information to a computer.
摘要翻译：用于测量眼睛运动的装置适用于独立的便携式使用，并适用于集成到头盔/头盔安装的显示器中。低成本非成像眼睛跟踪系统针对需要计算机光标控制的应用程序进行了优化，因为操作者通过固定框架来定位目视方向，以便向计算机提供指向信息。

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