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1. 发明申请

US20190027744A2 NEGATIVE ELECTRODE COMPOSITION FOR ELECTRIC STORAGE DEVICE, NEGATIVE ELECTRODE INCLUDING THE COMPOSITION, ELECTRIC STORAGE DEVICE, AND METHOD FOR PRODUCING NEGATIVE ELECTRODE FOR ELECTRIC STORAGE DEVICE 审中-公开
公开(公告)号：US20190027744A2
公开(公告)日：2019-01-24
申请号：US15526707
申请日：2015-11-12
申请人： Shinichi Maruyama , Koji Nitta , Shoichiro Sakai , Atsushi Fukunaga , Eiko Imazaki , Koma Numata , Hideaki Ito , Hitoshi Kobayashi , Toshiaki Yamashita , Shinichi Maruyama
发明人： Koji Nitta , Shoichiro Sakai , Atsushi Fukunaga , Eiko Imazaki , Koma Numata , Hideaki Ito , Hitoshi Kobayashi , Toshiaki Yamashita , Shinichi Maruyama
IPC分类号： H01M4/38 , H01M10/0564
CPC分类号： H01M4/381 , H01G11/04 , H01G11/30 , H01G11/62 , H01G11/86 , H01M4/0459 , H01M4/134 , H01M4/1395 , H01M4/362 , H01M10/054 , H01M10/0564 , H01M10/0566 , Y02E60/13
摘要： Provided is a method for producing a negative electrode for an electric storage device, the method comprising the steps of: preparing a negative electrode composition comprising a negative electrode active material that reversibly carries a sodium ion, metal sodium, and a liquid dispersion medium for dispersing them; allowing a negative electrode current collector to hold the negative electrode composition; evaporating at least part of the liquid dispersion medium from the negative electrode composition held by the negative electrode current collector, thereby giving a negative electrode precursor comprising the negative electrode active material, the metal sodium, and the negative electrode current collector; and bringing the negative electrode precursor into contact with an electrolyte having sodium ion conductivity, thereby doping the negative electrode active material with sodium eluted from the metal sodium.

2. 发明申请

US20180151877A2 NEGATIVE ELECTRODE COMPOSITION FOR ELECTRIC STORAGE DEVICE, NEGATIVE ELECTRODE INCLUDING THE COMPOSITION, ELECTRIC STORAGE DEVICE, AND METHOD FOR PRODUCING NEGATIVE ELECTRODE FOR ELECTRIC STORAGE DEVICE 审中-公开
公开(公告)号：US20180151877A2
公开(公告)日：2018-05-31
申请号：US15526707
申请日：2015-11-12
申请人： Shinichi Maruyama , Koji Nitta , Shoichiro Sakai , Atsushi Fukunaga , Eiko Imazaki , Koma Numata , Hideaki Ito , Hitoshi Kobayashi , Toshiaki Yamashita , Shinichi Maruyama
发明人： Koji Nitta , Shoichiro Sakai , Atsushi Fukunaga , Eiko Imazaki , Koma Numata , Hideaki Ito , Hitoshi Kobayashi , Toshiaki Yamashita
IPC分类号： H01M4/38 , H01M10/0564
CPC分类号： H01M4/381 , H01G11/04 , H01G11/30 , H01G11/62 , H01G11/86 , H01M4/0459 , H01M4/134 , H01M4/1395 , H01M4/362 , H01M10/054 , H01M10/0564 , H01M10/0566 , Y02E60/13
摘要： Provided is a method for producing a negative electrode for an electric storage device, the method comprising the steps of: preparing a negative electrode composition comprising a negative electrode active material that reversibly carries a sodium ion, metal sodium, and a liquid dispersion medium for dispersing them; allowing a negative electrode current collector to hold the negative electrode composition; evaporating at least part of the liquid dispersion medium from the negative electrode composition held by the negative electrode current collector, thereby giving a negative electrode precursor comprising the negative electrode active material, the metal sodium, and the negative electrode current collector; and bringing the negative electrode precursor into contact with an electrolyte having sodium ion conductivity, thereby doping the negative electrode active material with sodium eluted from the metal sodium.

3. 发明授权

US08324788B2 Piezoelectric power generator 有权
标题翻译：压电发电机
公开(公告)号：US08324788B2
公开(公告)日：2012-12-04
申请号：US13251314
申请日：2011-10-03
申请人： Eitaro Kameda , Toshiaki Yamashita
发明人： Eitaro Kameda , Toshiaki Yamashita
IPC分类号： H02N2/00 , H01L41/08
CPC分类号： H02N2/18 , B60C23/0411
摘要： A piezoelectric power generator having a first elastic body which deforms along a first direction when subject to a stress, and a power-generating element. The power-generating element includes a second elastic body and a piezoelectric element. The second elastic body includes a fixing portion and an abutting portion. The fixing portion is fixed to the first elastic body. The abutting portion is arranged on one side in a first direction with respect to the fixing portion. The abutting portion abuts against the first elastic body, but is not fixed to the first elastic body. At least one of the first elastic body and the second elastic body is provided with a slippage suppression mechanism that suppresses slipping of the abutting portion with respect to the first elastic body when the first elastic body is deformed.
摘要翻译：一种压电发电机，具有在受到应力时沿着第一方向变形的第一弹性体和发电元件。发电元件包括第二弹性体和压电元件。第二弹性体包括固定部和抵接部。固定部固定在第一弹性体上。抵接部相对于固定部沿第一方向配置在一侧。抵接部与第一弹性体抵接，但不固定于第一弹性体。第一弹性体和第二弹性体中的至少一个具有滑动抑制机构，当第一弹性体变形时，能够抑制抵接部相对于第一弹性体的滑动。

4. 发明申请

US20120043856A1 Piezoelectric Power Generator 有权
标题翻译：压电发电机
公开(公告)号：US20120043856A1
公开(公告)日：2012-02-23
申请号：US13251314
申请日：2011-10-03
申请人： Eitaro Kameda , Toshiaki Yamashita
发明人： Eitaro Kameda , Toshiaki Yamashita
IPC分类号： H01L41/113 , H01L41/04
CPC分类号： H02N2/18 , B60C23/0411
摘要： A piezoelectric power generator having a first elastic body which deforms along a first direction when subject to a stress, and a power-generating element. The power-generating element includes a second elastic body and a piezoelectric element. The second elastic body includes a fixing portion and an abutting portion. The fixing portion is fixed to the first elastic body. The abutting portion is arranged on one side in a first direction with respect to the fixing portion. The abutting portion abuts against the first elastic body, but is not fixed to the first elastic body. At least one of the first elastic body and the second elastic body is provided with a slippage suppression mechanism that suppresses slipping of the abutting portion with respect to the first elastic body when the first elastic body is deformed.
摘要翻译：一种压电发电机，具有在受到应力时沿着第一方向变形的第一弹性体和发电元件。发电元件包括第二弹性体和压电元件。第二弹性体包括固定部和抵接部。固定部固定在第一弹性体上。抵接部相对于固定部沿第一方向配置在一侧。抵接部与第一弹性体抵接，但不固定于第一弹性体。第一弹性体和第二弹性体中的至少一个具有滑动抑制机构，当第一弹性体变形时，能够抑制抵接部相对于第一弹性体的滑动。

5. 发明授权

US5838278A Antenna pointing apparatus mounted on satellite using feed forward with reference model 失效
标题翻译：使用前馈参考模型安装在卫星上的天线指向装置
公开(公告)号：US5838278A
公开(公告)日：1998-11-17
申请号：US735882
申请日：1996-10-23
申请人： Takahiko Tsujisawa , Toshiaki Yamashita
发明人： Takahiko Tsujisawa , Toshiaki Yamashita
IPC分类号： B64G1/66 , B64G3/00 , G05D3/12 , H01Q1/18 , H01Q3/00 , H01Q3/04 , H01Q3/08 , H04B7/185 , H04B10/07 , H04B10/11 , H04B10/118
CPC分类号： H01Q1/18 , H01Q3/08
摘要： An optical antenna pointing controller for an optical antenna system having an optical antenna and biaxial gimbal mechanism coupled to the optical antenna and mounted on the satellite is provided. Feedback control in the controller is gain-stabilized by a nominal compensator, and disturbance is suppressed by a robust compensator, further, a target satellite is captured quickly with the aid of a reference model and feedforward, thus providing quick response without dependency on the band width of feedback control system.
摘要翻译：提供了一种用于具有耦合到光学天线并安装在卫星上的光学天线和双轴万向架机构的光学天线系统的光学天线指向控制器。控制器中的反馈控制由标称补偿器增益稳定，并且由鲁棒补偿器抑制干扰，此外，借助参考模型和前馈快速捕获目标卫星，从而提供快速响应，而不依赖于频带反馈控制系统的宽度。

6. 发明申请

US20050193277A1 Apparatus, method, and program for correcting time of event trace data 有权
标题翻译：用于校正事件跟踪数据时间的装置，方法和程序
公开(公告)号：US20050193277A1
公开(公告)日：2005-09-01
申请号：US11062930
申请日：2005-02-23
申请人： Takashi Horikawa , Toshiaki Yamashita
发明人： Takashi Horikawa , Toshiaki Yamashita
IPC分类号： G06F11/34 , G06F11/00
CPC分类号： G06F11/3495 , G06F11/3476 , G06F2201/875
摘要： A time correcting apparatus includes a data input section which inputs all event trace data generated for each event executed on computing devices and outputs the event trace data in order of occurrence time of the event data. An inter-machine communication-time-table generating section extracts transmission and reception events from the output event trace data and generates a communication time table indicating communication times between computing devices based on the differences in occurrence time between the corresponding transmission and reception events. A time-offset deriving section generates a time offset table indicating a time offset value for each computing device based on the communication time table. A time correcting section corrects the event occurrence times of all event data based on the time offset table. A data integrating section inputs all event data whose occurrence times have been corrected and outputs the event data in order of corrected occurrence time.
摘要翻译：时间校正装置包括数据输入部分，其输入为在计算装置上执行的每个事件生成的所有事件跟踪数据，并且以事件数据的发生时间的顺序输出事件跟踪数据。机间通信时间表生成部从输出事件跟踪数据中提取发送接收事件，根据相应的发送接收事件的发生时间的差异，生成指示计算装置之间的通信时间的通信时间表。时间偏移导出部根据通信时间表生成表示各计算装置的时间偏移值的时间偏移表。时间校正部根据时间偏移表来校正所有事件数据的事件发生次数。数据积分部分输入发生时间已被校正的所有事件数据，并按照校正发生时间的顺序输出事件数据。

7. 发明授权

US06622969B2 Maneuver device for artificial satellite 有权
标题翻译：人造卫星机动装置
公开(公告)号：US06622969B2
公开(公告)日：2003-09-23
申请号：US10078109
申请日：2002-02-20
申请人： Toshiaki Yamashita
发明人： Toshiaki Yamashita
IPC分类号： B64G128
CPC分类号： G05D1/0883 , B64G1/26 , B64G1/283 , B64G2001/245
摘要： The present invention provides a maneuver device for an artificial satellite, which causes small attitude error during maneuver and which requires a shorter period of setting time for obtaining a target attitude. The maneuver device is provided with: a feed forward torque instruction signal generator 8 which outputs a feed forward torque instruction signal 11 based on a maneuver plan; a thruster 10 which outputs control torque based on the feed forward torque instruction signal 11; and an attitude control signal calculator 6 to which an attitude angle and an angular velocity of the artificial satellite as well as a target attitude angle and a target angular velocity are input and which outputs an attitude control signal 13. The maneuver device is further provided with a disturbance compensating signal calculator to which the feed forward torque instruction signal 11 and a detected angular velocity signal 16 are input, and which generates and outputs a disturbance compensating signal 12. The maneuver device is yet further provided with a reaction wheel 7 which generates control torque based on the attitude control signal 13 and the disturbance compensating signal 12.
摘要翻译：本发明提供了一种用于人造卫星的操纵装置，其在操纵期间导致小的姿态误差，并且需要较短的设定时间来获得目标姿态。机动装置设置有：前馈转矩指令信号发生器8，基于机动计划输出前馈转矩指令信号11; 基于前馈转矩指令信号11输出控制转矩的推进器10; 并且输入人造卫星的姿态角和角速度以及目标姿态角和目标角速度的姿态控制信号计算器6，并且输出姿态控制信号13.该操纵装置还设置有输入前馈转矩指令信号11和检测角速度信号16的干扰补偿信号计算器，并产生并输出干扰补偿信号12.该机动装置还具备反作用轮7，其产生控制基于姿态控制信号13和干扰补偿信号12的转矩。

8. 发明授权

US06574534B2 6-degree-of-freedom control apparatus for spacecraft 有权
公开(公告)号：US06574534B2
公开(公告)日：2003-06-03
申请号：US09536812
申请日：2000-03-28
申请人： Toshiaki Yamashita
发明人： Toshiaki Yamashita
IPC分类号： B64C100
CPC分类号： B64G1/26 , G05D1/0883
摘要： A 6-degree-of-freedom control apparatus for a spacecraft includes a plurality of thrusters, thruster modulator, position/velocity detector, target position/velocity generator, attitude/angular velocity detector, target attitude/angular velocity generator, and 6-degree-of-freedom controller. The thrusters control three position axes and three attitude axes of a spacecraft by jet. The thruster modulator selectively drives the thrusters on the basis of a thruster control signal. The position/velocity detector measures a position and velocity of the spacecraft. The target position/velocity generator generates target position and velocity values of the spacecraft. The attitude/angular velocity detector measures an attitude and angular velocity of the spacecraft. The target attitude/angular velocity generator generates target attitude and angular velocity values of the spacecraft. The 6-degree-of-freedom controller generates the thruster control signal on the basis of a deviation between an output from the position/velocity detector and an output from the target position/velocity generator and a deviation between an output from the attitude/angular velocity detector and an output from the target attitude/angular velocity generator and outputs the signal to the thruster modulator.

9. 发明授权

US06336062B1 Attitude angle sensor correcting apparatus for an artificial satellite 有权
标题翻译：用于人造卫星的姿态角传感器校正装置
公开(公告)号：US06336062B1
公开(公告)日：2002-01-01
申请号：US09731028
申请日：2000-12-07
申请人： Toshiaki Yamashita
发明人： Toshiaki Yamashita
IPC分类号： G06F1740
CPC分类号： B64G1/365 , B64G1/1021 , B64G1/66 , B64G2001/245
摘要： An attitude angle sensor correcting apparatus for an artificial satellite of the present invention includes a satellite attitude estimator. The satellite attitude estimator reads geographical image data out of an image data memory, produces a GCP (Ground Control Point) position included in the image data by stereo image measurement, and then estimates the instantaneous satellite attitude angle on the basis of a relation between the measured GCP position and a true GCP position. An attitude angle sensor data corrector corrects measured attitude angle data with estimated satellite attitude data output from the satellite attitude estimator and corresponding in time to the measured attitude angle data. The attitude angle sensor data corrector outputs an estimated satellite attitude signal.
摘要翻译：本发明的人造卫星姿态角度传感器校正装置包括卫星姿态估计器。卫星姿态估计器从图像数据存储器读取地理图像数据，通过立体图像测量产生包括在图像数据中的GCP（地面控制点）位置，然后基于测量GCP位置和真实的GCP位置。姿态角传感器数据校正器将测量的姿态角数据与从卫星姿态估计器输出的估计的卫星姿态数据相对应地对准测量的姿态角数据。姿态角传感器数据校正器输出估计卫星姿态信号。

10. 发明授权

US5629709A Tracking control device of antenna loaded on movable body and tracking control method of the antenna 失效
标题翻译：天线加载跟踪控制装置和天线跟踪控制方法
公开(公告)号：US5629709A
公开(公告)日：1997-05-13
申请号：US333046
申请日：1994-11-01
申请人： Toshiaki Yamashita
发明人： Toshiaki Yamashita
IPC分类号： H01Q3/02 , G01S3/42 , H01Q1/12 , H01Q1/32 , H01Q3/10 , H01Q3/00
CPC分类号： H01Q3/10 , H01Q1/1257 , H01Q1/3233
摘要： An antenna tracking control device includes detectors for detecting speed and the steering angle of a movable body, a device for calculating the estimated azimuth angle of the movable body based on the detected speed and steering angle, and a detector for detecting the azimuth angle of the movable body. Also, an azimuth angle error estimator is provided for calculating the error between the calculated estimated azimuth angle and the detected azimuth angle. In addition, a directing angle error detector is used for detecting antenna directing angle error, and a directing angle error corrector is used for correcting the detected antenna directing angle error, with the result that the antenna tracking control device causes an antenna mounted on a moveable body, such as an automobile, to track a wave generating source based on the corrected antenna directing angle error.
摘要翻译：天线跟踪控制装置包括用于检测可移动体的速度和转向角的检测器，用于基于检测到的速度和转向角计算可移动体的估计方位角的装置，以及用于检测可移动体的方位角的检测器移动体。此外，提供了一种方位角误差估计器，用于计算所计算的估计方位角和检测到的方位角之间的误差。另外，引导角度误差检测器用于检测天线指向角度误差，并且使用定向角误差校正器来校正检测到的天线指向角度误差，结果是天线跟踪控制装置使安装在可移动的天线基于校正的天线指向角度误差跟踪波发生源。

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