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1. 发明授权

US08038101B2 Attitude change control method, attitude change control system, attitude change control program and program recording medium 有权
标题翻译：姿态改变控制方法，姿态变化控制系统，姿态变化控制程序和程序记录介质
公开(公告)号：US08038101B2
公开(公告)日：2011-10-18
申请号：US12027769
申请日：2008-02-07
申请人： Keita Ogo , Toshio Kamiya , Ken Maeda
发明人： Keita Ogo , Toshio Kamiya , Ken Maeda
IPC分类号： B64G1/28
CPC分类号： B64G1/286 , G05D1/0883
摘要： Disclosed is an attitude change control system that is designed to efficiently output a torque for attitude change of a space craft using CMGs and realizes a real time CMG driving rule. A CMG gimbal steering law 15 generates target profiles for setting angle and angular velocity for each gimbal by applying an anisotropic weighted gradient method based upon the necessary torque calculated by a feed back controller 13 and a feed forward controller 14 from the angle and angular velocity in the target direction from the attitude navigator 12 and the current angle and angular velocity of the space craft estimated by the attitude estimator 11 as well as the current condition of each gimbal from the CMG 40, thereby controlling the CMG 40 for changing the attitude of the space craft dynamics 50 to the target direction.
摘要翻译：公开了一种姿态改变控制系统，其被设计为有效地输出用于使用CMG的航天飞机姿态变化的扭矩并实现实时CMG驱动规则。 CMG万向节转向规则15通过基于由反馈控制器13和前馈控制器14计算出的必要扭矩，通过从角度和角速度来计算每个万向节的角度和角速度来生成用于设置每个万向节的角度和角速度的目标轮廓来自姿态导航仪12的目标方向以及由姿态估计器11估计的航天飞船的当前角度和角速度以及来自CMG 40的每个万向节的当前状态，从而控制CMG 40改变姿态太空工艺动力50目标方向。

2. 发明申请

US20090039202A1 Attitude Change Control Method, Attitude Change Control System, Attitude Change Control Program and Program Recording Medium 审中-公开
标题翻译：态度变化控制方法，态度变化控制系统，态度变化控制程序和程序记录介质
公开(公告)号：US20090039202A1
公开(公告)日：2009-02-12
申请号：US12191389
申请日：2008-08-14
申请人： Keita Ogo , Toshio Kamiya , Ken Maeda
发明人： Keita Ogo , Toshio Kamiya , Ken Maeda
IPC分类号： B64G1/28 , B64G1/24
CPC分类号： B64G1/286 , B64G2001/245
摘要： Disclosed is an attitude change control system that is designed to efficiently output a torque for attitude change of a space craft using CMGs and realizes a real time CMG driving rule. A CMG gimbal steering law 15 generates target profiles for setting angle and angular velocity for each gimbal by applying an anisotropic weighted gradient method based upon the necessary torque calculated by a feed back controller 13 and a feed forward controller 14 from the angle and angular velocity in the target direction from the attitude navigator 12 and the current angle and angular velocity of the space craft estimated by the attitude estimator 11 as well as the current condition of each gimbal from the CMG 40, thereby controlling the CMG 40 for changing the attitude of the space craft dynamics 50 to the target direction.
摘要翻译：公开了一种姿态改变控制系统，其被设计为有效地输出用于使用CMG的航天飞机姿态变化的扭矩并实现实时CMG驱动规则。 CMG万向节转向规则15通过基于由反馈控制器13和前馈控制器14计算出的必要扭矩，通过从角度和角速度来计算每个万向节的角度和角速度来生成用于设置每个万向节的角度和角速度的目标轮廓来自姿态导航仪12的目标方向以及由姿态估计器11估计的航天飞船的当前角度和角速度以及来自CMG 40的每个万向节的当前状态，从而控制CMG 40改变姿态太空工艺动力50目标方向。

3. 发明申请

US20080203230A1 ATTITUDE CHANGE CONTROL METHOD, ATTITUDE CHANGE CONTROL SYSTEM, ATTITUDE CHANGE CONTROL PROGRAM AND PROGRAM RECORDING MEDIUM 有权
标题翻译：态度变化控制方法，态度变化控制系统，态度变化控制程序和程序记录介质
公开(公告)号：US20080203230A1
公开(公告)日：2008-08-28
申请号：US12027769
申请日：2008-02-07
申请人： KEITA OGO , Toshio Kamiya , Ken Maeda
发明人： KEITA OGO , Toshio Kamiya , Ken Maeda
IPC分类号： B64G1/28
CPC分类号： B64G1/286 , G05D1/0883
摘要： Disclosed is an attitude change control system that is designed to efficiently output a torque for attitude change of a space craft using CMGs and realizes a real time CMG driving rule. A CMG gimbal steering law 15 generates target profiles for setting angle and angular velocity for each gimbal by applying an anisotropic weighted gradient method based upon the necessary torque calculated by a feed back controller 13 and a feed forward controller 14 from the angle and angular velocity in the target direction from the attitude navigator 12 and the current angle and angular velocity of the space craft estimated by the attitude estimator 11 as well as the current condition of each gimbal from the CMG 40, thereby controlling the CMG 40 for changing the attitude of the space craft dynamics 50 to the target direction.
摘要翻译：公开了一种姿态改变控制系统，其被设计为有效地输出用于使用CMG的航天飞机姿态变化的扭矩并实现实时CMG驱动规则。 CMG万向节转向规则15通过基于由反馈控制器13和前馈控制器14计算出的必要扭矩，通过从角度和角速度来计算每个万向节的角度和角速度来生成用于设置每个万向节的角度和角速度的目标轮廓来自姿态导航仪12的目标方向以及由姿态估计器11估计的航天飞船的当前角度和角速度以及来自CMG 40的每个万向节的当前状态，从而控制CMG 40改变姿态太空工艺动力50目标方向。

4. 发明授权

US08186627B2 Attitude control data creating method, and attitude control system applying the method 有权
标题翻译：态度控制数据创建方法，姿态控制系统应用该方法
公开(公告)号：US08186627B2
公开(公告)日：2012-05-29
申请号：US12300449
申请日：2007-05-02
申请人： Toshio Kamiya , Ken Maeda , Tatsuaki Hashimoto , Shinichiro Sakai
发明人： Toshio Kamiya , Ken Maeda , Tatsuaki Hashimoto , Shinichiro Sakai
IPC分类号： B64G1/36
CPC分类号： B64G1/24 , B64G1/283 , B64G1/286 , B64G1/36 , B64G1/38 , G05D1/0883
摘要： In order to control an attitude of a movable object having a flexible member (50) through an attitude maneuver, first, based on vibration of the flexible member at the time of the attitude maneuver, for example, a sampling function including no frequency components equal to or higher than a particular frequency is obtained. With the use of the sampling function, a control target value is created as a previously-frequency-shaping-type feedforward control law. Based on the control target value, attitude control data is created. The attitude control data can be used for the attitude maneuver with respect to the movable object.
摘要翻译：为了通过姿态机动来控制具有柔性构件（50）的可移动物体的姿态，首先，基于姿态机动时的柔性构件的振动，例如，不包括频率成分相等的取样函数达到或高于特定频率。利用采样功能，创建控制目标值作为先前频率整形型的前馈控制定律。基于控制目标值，创建姿态控制数据。姿态控制数据可以用于相对于可移动物体的姿态操纵。

5. 发明申请

US20090218449A1 ATTITUDE CONTROL DATA CREATING METHOD, AND ATTITUDE CONTROL SYSTEM APPLYING THE METHOD 有权
标题翻译：态度控制数据创建方法以及应用方法的态度控制系统
公开(公告)号：US20090218449A1
公开(公告)日：2009-09-03
申请号：US12300449
申请日：2007-05-02
申请人： Toshio Kamiya , Ken Maeda , Tatsuaki Hashimoto , Shinichiro Sakai
发明人： Toshio Kamiya , Ken Maeda , Tatsuaki Hashimoto , Shinichiro Sakai
IPC分类号： B64G1/28 , B64G1/24
CPC分类号： B64G1/24 , B64G1/283 , B64G1/286 , B64G1/36 , B64G1/38 , G05D1/0883
摘要： In order to control an attitude of a movable object having a flexible member (50) through an attitude maneuver, first, based on vibration of the flexible member at the time of the attitude maneuver, for example, a sampling function including no frequency components equal to or higher than a particular frequency is obtained. With the use of the sampling function, a control target value is created as a previously-frequency-shaping-type feedforward control law. Based on the control target value, attitude control data is created. The attitude control data can be used for the attitude maneuver with respect to the movable object.
摘要翻译：为了通过姿态机动来控制具有柔性构件（50）的可移动物体的姿态，首先，基于姿态机动时的柔性构件的振动，例如，不包括频率成分相等的取样函数达到或高于特定频率。利用采样功能，创建控制目标值作为先前频率整形型的前馈控制定律。基于控制目标值，创建姿态控制数据。姿态控制数据可以用于相对于可移动物体的姿态操纵。

6. 发明授权

US09947803B2 Amorphous oxide and thin film transistor 有权
公开(公告)号：US09947803B2
公开(公告)日：2018-04-17
申请号：US13097572
申请日：2011-04-29
申请人： Hideo Hosono , Masahiro Hirano , Hiromichi Ota , Toshio Kamiya , Kenji Nomura
发明人： Hideo Hosono , Masahiro Hirano , Hiromichi Ota , Toshio Kamiya , Kenji Nomura
IPC分类号： H01L21/336 , H01L29/786 , C23C14/00 , C23C14/08 , C23C14/28 , C23C14/34 , H01L21/02 , H01L27/12
CPC分类号： H01L29/78696 , C23C14/0021 , C23C14/086 , C23C14/28 , C23C14/3414 , H01L21/02554 , H01L21/02565 , H01L21/02631 , H01L27/1225 , H01L29/7869 , H01L29/78693
摘要： The present invention relates to an amorphous oxide and a thin film transistor using the amorphous oxide. In particular, the present invention provides an amorphous oxide having an electron carrier concentration less than 1018/cm3, and a thin film transistor using such an amorphous oxide. In a thin film transistor having a source electrode 6, a drain electrode 5, a gate electrode 4, a gate insulating film 3, and a channel layer 2, an amorphous oxide having an electron carrier concentration less than 1018/cm3 is used in the channel layer 2.

7. 发明授权

US09269826B2 Amorphous oxide and thin film transistor 有权
标题翻译：无定形氧化物和薄膜晶体管
公开(公告)号：US09269826B2
公开(公告)日：2016-02-23
申请号：US12984960
申请日：2011-01-05
申请人： Hideo Hosono , Masahiro Hirano , Hiromichi Ota , Toshio Kamiya , Kenji Nomura
发明人： Hideo Hosono , Masahiro Hirano , Hiromichi Ota , Toshio Kamiya , Kenji Nomura
IPC分类号： H01L29/786 , C23C14/00 , C23C14/08 , C23C14/28 , C23C14/34 , H01L21/02 , H01L27/12
CPC分类号： H01L29/78696 , C23C14/0021 , C23C14/086 , C23C14/28 , C23C14/3414 , H01L21/02554 , H01L21/02565 , H01L21/02631 , H01L27/1225 , H01L29/7869 , H01L29/78693
摘要： The present invention relates to an amorphous oxide and a thin film transistor using the amorphous oxide. In particular, the present invention provides an amorphous oxide having an electron carrier concentration less than 1018/cm3, and a thin film transistor using such an amorphous oxide. In a thin film transistor having a source electrode 6, a drain electrode 5, a gate electrode 4, a gate insulating film 3, and a channel layer 2, an amorphous oxide having an electron carrier concentration less than 1018/cm3 is used in the channel layer 2.
摘要翻译：本发明涉及使用该无定形氧化物的无定形氧化物和薄膜晶体管。特别地，本发明提供了电子载流子浓度小于1018 / cm3的非晶氧化物，以及使用这种无定形氧化物的薄膜晶体管。在具有源电极6，漏电极5，栅电极4，栅极绝缘膜3和沟道层2的薄膜晶体管中，使用电子载流子浓度小于1018 / cm3的非晶氧化物通道层2。

8. 发明授权

US08435473B2 Superconducting compound and method for producing the same 有权
标题翻译：超导化合物及其制造方法
公开(公告)号：US08435473B2
公开(公告)日：2013-05-07
申请号：US12865940
申请日：2009-02-17
申请人： Hideo Hosono , Yoichi Kamihara , Masahiro Hirano , Toshio Kamiya , Hiroshi Yanagi
发明人： Hideo Hosono , Yoichi Kamihara , Masahiro Hirano , Toshio Kamiya , Hiroshi Yanagi
IPC分类号： C01F17/00 , C01B25/10 , C01B15/16 , C01B25/26 , C01B21/20 , C01B13/00 , C01C1/00 , C01D1/02 , C01G49/00 , C01G53/04 , C01G29/00 , C01G30/00 , C01G28/02 , C01G28/00
CPC分类号： C01G53/006 , C01G49/009 , C01G55/002 , C01P2002/52 , C01P2002/72 , C01P2002/76 , C01P2002/78 , C01P2002/88 , C01P2006/40 , C01P2006/42 , C04B35/447 , C04B2235/3208 , C04B2235/3225 , C04B2235/3227 , C04B2235/3229 , C04B2235/3279 , C04B2235/40 , C04B2235/405 , C04B2235/42 , C04B2235/445 , H01L39/125
摘要： Disclosed is a superconducting compound which has a structure obtained by partially substituting oxygen ions of a compound, which is represented by the following chemical formula; LnTMOPh [wherein Ln represents at least one element selected from Y and rare earth metal elements (La, Ce, Pr, Nd, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb and Lu), TM represents at least one element selected from transition metal elements (Fe, Ru, Os, Ni, Pd and Pt), and Pn represents at least one element selected from pnictide elements (N, P, As and Sb)] and has a ZrCuSiAs-type crystal structure (space group P4/nmm), with at least one kind of monovalent anion (F−, Cl− or Br−). The superconducting compound alternatively has a structure obtained by partially substituting Ln ions of the compound with at least one kind of tetravalent metal ion (Ti4+, Zr4+, Hf4+, C4+, Si4+, Ge4+, Sn4+ or Pb4+) or a structure obtained by partially substituting Ln ions of the compound with at least one kind of divalent metal ion (Mg2+, Ca2+, Sr2+ or Ba2+). The Tc of the superconducting compound is controlled in accordance with the ion substitution amount.
摘要翻译：公开了一种超导化合物，其具有通过部分取代由以下化学式表示的化合物的氧离子而获得的结构; LnTMOPh [其中Ln表示选自Y和稀土金属元素（La，Ce，Pr，Nd，Sm，Eu，Gd，Tb，Dy，Ho，Er，Tm，Yb和Lu）中的至少一种元素，TM表示选自过渡金属元素（Fe，Ru，Os，Ni，Pd和Pt）中的至少一种元素，Pn表示选自铌元素（N，P，As和Sb）中的至少一种元素]，并且具有ZrCuSiAs型晶体结构（空间群P4 / nmm），具有至少一种一价阴离子（F-，Cl-或Br-）。超导化合物或者具有通过用至少一种四价金属离子（Ti 4+，Zr 4+，Hf 4+，C 4+，Si 4+，Ge 4+，Sn 4+或Pb 4+）部分取代化合物的Ln离子或通过部分取代Ln而获得的结构化合物与至少一种二价金属离子（Mg2 +，Ca2 +，Sr2 +或Ba2 +）的离子。超导化合物的Tc根据离子取代量进行控制。

9. 发明授权

US08288321B2 Layered compound, superconductor and method for producing same 有权
标题翻译：层状化合物，超导体及其制造方法
公开(公告)号：US08288321B2
公开(公告)日：2012-10-16
申请号：US13003149
申请日：2009-07-09
申请人： Hideo Hosono , Hiroshi Yanagi , Toshio Kamiya , Satoru Matsuishi , Sungwng Kim , Seok Gyu Yoon , Hidenori Hiramatsu , Masahiro Hirano , Takatoshi Nomura , Yoichi Kamihara
发明人： Hideo Hosono , Hiroshi Yanagi , Toshio Kamiya , Satoru Matsuishi , Sungwng Kim , Seok Gyu Yoon , Hidenori Hiramatsu , Masahiro Hirano , Takatoshi Nomura , Yoichi Kamihara
IPC分类号： C04B35/45
CPC分类号： C01G49/009 , C01G53/006 , C01G55/002 , C01P2002/34 , C01P2002/52 , C01P2002/72 , C01P2002/76 , C01P2002/77 , C01P2002/78 , C01P2004/61 , C01P2004/80 , C01P2006/40 , C01P2006/42 , C04B35/515 , C04B35/5154 , C04B35/553 , C04B2235/3208 , C04B2235/3213 , C04B2235/40 , C04B2235/401 , C04B2235/405 , C04B2235/445 , C04B2235/446 , C04B2235/5436 , C04B2235/6581 , C04B2235/76 , H01L39/125
摘要： Provides a new non-oxide system compound material superconductor as an alternative of the perovskite type copper oxides superconductor.Layered compounds which are represented by chemical formula AF(TM)Pn (wherein, A is at least one selected from a group consisting of the second family elements in the long form periodic table, F is a fluorine ion, TM is at least one selected from a group of transition metal elements consisting of Fe, Ru, Os, Ni, Pd, and Pt, and Pn is at least one selected from a group consisting of the fifteenth family elements in the long form periodic table), having a crystal structure of ZrCuSiAs type (space group P4/nmm) and which become superconductors by doping trivalent cations or divalent anions.
摘要翻译：提供新的非氧化物系复合材料超导体作为钙钛矿型铜氧化物超导体的替代品。由化学式AF（TM）Pn表示的分层化合物（其中，A是选自长型周期表中的第二族元素的F中的至少一种，F是氟离子，TM是至少一种选择的由一组由Fe，Ru，Os，Ni，Pd和Pt组成的过渡金属元素，Pn是选自由长型周期表中的第十五族系元素组成的组中的至少一种），具有晶体结构的ZrCuSiAs型（空间群P4 / nmm），通过掺杂三价阳离子或二价阴离子成为超导体。

10. 发明授权

US07829444B2 Field effect transistor manufacturing method 有权
标题翻译：场效应晶体管制造方法
公开(公告)号：US07829444B2
公开(公告)日：2010-11-09
申请号：US11269641
申请日：2005-11-09
申请人： Hisato Yabuta , Masafumi Sano , Tatsuya Iwasaki , Hideo Hosono , Toshio Kamiya , Kenji Nomura
发明人： Hisato Yabuta , Masafumi Sano , Tatsuya Iwasaki , Hideo Hosono , Toshio Kamiya , Kenji Nomura
IPC分类号： H01L21/20
CPC分类号： H01L29/78618 , H01L29/66969 , H01L29/78693
摘要： Provided is a novel method for manufacturing a field effect transistor. Prior to forming an amorphous oxide layer on a substrate, ultraviolet rays are irradiated onto the substrate surface in an ozone atmosphere, plasma is irradiated onto the substrate surface, or the substrate surface is cleaned by a chemical solution containing hydrogen peroxide.
摘要翻译：提供一种用于制造场效应晶体管的新颖方法。在基板上形成无定形氧化物层之前，在臭氧气氛中将紫外线照射到基板表面上，将等离子体照射到基板表面上，或者通过含有过氧化氢的化学溶液清洁基板表面。

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