101. 人造衛星天線

申请号: TW077305887

申请日: 1988-10-11

公开（公告）号: TW119026S

公开（公告）日: 1989-09-11

发明人: 派崔克.坎貝爾.亨特

102. Panel type artificial satellite and artificial satellite system therewith

申请号: EP11165796.1

申请日: 2011-05-12

公开（公告）号: EP2386489A2

公开（公告）日: 2011-11-16

发明人: Takahashi, Tadayuki; Takashima, Takeshi; Ogawa, Hiroyuki; Sakai, Shin-ichiro; Iwata, Naoko; Kuroda, Yoshikatsu; Masukawa, Kazunori

An artificial satellite system (200) comprises at least two panel type artificial satellites (100) closely connected with a plurality kind of multi networks and the minimum necessary essential tools for one artificial satellite installed on a substrate of each panel type artificial satellites (100), wherein the multi networks(N1, N2, N3) are formed by a communicating network for communicating data among data processing tools installed on each the panel type artificial satellites (100), a heat pipe for providing thermal energy among tools installed on each the panel type artificial satellites (100) and a battery supplying line for connecting battery controlling devices installed in the each panel type artificial satellite so that the artificial satellite system (200) can maintain higher and various controlling performance with a back-up effect of the multi network in the case that any function tool is damaged in one of the panel type artificial satellite (100).

103. Maneuver device for artificial satellite

申请号: US10078109

申请日: 2002-02-20

公开（公告）号: US20020148930A1

公开（公告）日: 2002-10-17

发明人: Toshiaki Yamashita

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.

104. ERGONOMIC SEATING ASSEMBLIES AND METHODS

申请号: US15261543

申请日: 2016-09-09

公开（公告）号: US20170065087A1

公开（公告）日: 2017-03-09

发明人: Nicholas M. Christianson; Jean Francois Gomrée; Rodney C. Schoenfelder; Jeffrey Weber; Shawn Monitor

Seating assemblies and methods are disclosed. A seating assembly can comprise a seat, a back support, and a frame component. The frame component can extend from a bottom portion, positioned near an underside of the seat, to a top portion, configured to maintain the back support at a position above the seat. The back support can laterally extend from a left edge portion to a right edge portion and can include a spring member at or near each of the left and right edge portions. The spring member can include at least one undulation or are providing integrated compression adaptation to a user. The seating assembly can further comprise a tilt mechanism, engaged with the frame component, including one or more leaf springs and a spring contact assembly. The spring contact assembly can be positioned on a top side of the one or more leaf springs.

105. ARTIFICIAL SATELLITE WITH INTEGRATED ANTENNA

申请号: US14353543

申请日: 2012-10-31

公开（公告）号: US20140292594A1

公开（公告）日: 2014-10-02

发明人: Tatsuji Moriguchi

An artificial satellite includes at least one hatch formed in a wall of the artificial satellite coming in contact with dead space of the artificial satellite, and a hatch opening and closing mechanism which opens the hatch, and the antenna is attached to the hatch.

106. ERGONOMIC SEATING ASSEMBLIES AND METHODS

申请号: PCT/US2012/049599

申请日: 2012-08-03

公开（公告）号: WO2013020088A2

公开（公告）日: 2013-02-07

发明人: CHRISTIANSON, Nicholas, M.; GOMREE, Jean Francois; SCHOENFELDER, Rodney, C.; WEBER, Jeffrey; MONITOR, Shawn

Seating assemblies and methods are disclosed. A seating assembly can comprise a seat, a back support, and a frame component. The frame component can extend from a bottom portion, positioned near an underside of the seat, to a top portion, configured to maintain the back support at a position above the seat. The back support can laterally extend from a left edge portion to a right edge portion and can include a spring member at or near each of the left and right edge portions. The spring member can include at least one undulation or arc providing integrated compression adaptation to a user. The seating assembly can further comprise a tilt mechanism, engaged with the frame component, including one or more leaf springs and a spring contact assembly. The spring contact assembly can be positioned on a top side of the one or more leaf springs.

107. Sandwich panel, and structural panel of artificial satellite

申请号: JP2004170138

申请日: 2004-06-08

公开（公告）号: JP2005349874A

公开（公告）日: 2005-12-22

发明人: HAHN STEVEN; UMADONO SHINJI; USAMI AKIRA; YAMAMOTO KAZUYUKI; OZAKI TAKESHI

PROBLEM TO BE SOLVED: To provide a circuit built-in sandwich panel consisting of a first skin, a second skin, and a core located between these two skins which is coexistent with a conventional surface mount of an electronic instrument or the like, capable of realizing integration and consolidation with the instrument, and a structure of a wire harness, a satellite or the like, and reducing the size, weight, and cost of the satellite, and a structural panel of the artificial satellite. SOLUTION: At least one (4a, 4b) of components or elements of an electronic circuit or an optical circuit and instruments related thereto is arranged in spaces (2a, 2b) provided in advance inside a core 8 located between two skins (1A, 1B). COPYRIGHT: (C)2006,JPO&NCIPI

108. ERGONOMIC SEATING ASSEMBLIES AND METHODS

申请号: PCT/US2012049599

申请日: 2012-08-03

公开（公告）号: WO2013020088A3

公开（公告）日: 2013-06-13

发明人: CHRISTIANSON NICHOLAS M; GOMREE JEAN FRANCOIS; SCHOENFELDER RODNEY C; WEBER JEFFREY; MONITOR SHAWN

Seating assemblies and methods are disclosed. A seating assembly (100) can comprise a seat, a back support (114), and a frame component (110). The frame component can extend from a bottom portion (118), positioned near an underside of the seat, to a top portion (120), configured to maintain the back support at a position above the seat. The back support can laterally extend from a left edge portion (1670) to a right edge portion (1672) and can include a spring member (122) at or near each of the left and right edge portions. The spring member can include at least one undulation or arc (1674) providing integrated compression adaptation to a user. The seating assembly can further comprise a tilt mechanism (408), engaged with the frame component, including one or more leaf springs (424) and a spring contact assembly. The spring contact assembly (426) can be positioned on a top side of the one or more leaf springs.

109. アンテナ内蔵型人工衛星

申请号: PCT/JP2012/078134

申请日: 2012-10-31

公开（公告）号: WO2013065722A1

公开（公告）日: 2013-05-10

发明人: 森口　達次

　人工衛星は、そのデッドスペースに接する当該人工衛星の壁に形成された少なくとも１つのハッチと、ハッチを開くハッチ開閉機構と、を備え、ハッチにアンテナが取付けられている。

110. Artificial satellite equipment panel

申请号: US11534684

申请日: 2006-09-25

公开（公告）号: US07619326B2

公开（公告）日: 2009-11-17

发明人: Hajime Takeya; Tsuyoshi Ozaki; Hirotsugu Morinaga; Shinji Badono

A satellite equipment panel on which may be mounted an installation equipment of a predetermined function, connectable by an interface, constitutes an artificial satellite. The satellite equipment panel includes a panel body, at least two interfaces for an interconnection to another satellite equipment panel, a line transfer switch disposed within the panel body for line transferring of the interconnection between the interfaces, wiring disposed within the panel body and connected at one end to one of the interfaces and at the other end to the line transfer switch for interconnecting the interfaces on that panel body. The interfaces and the wiring, in cooperation with a support structure, constitute a wiring module disposed within the panel body. The interface may comprise at least one of interfaces of electric communication, optical communication, and optical sensor.

111. Simulated orbiting artificial satellite

申请号: US72607958

申请日: 1958-04-03

公开（公告）号: US2897607A

公开（公告）日: 1959-08-04

发明人: PARK ALEXANDER C

112. Magnetic bearing arrangement for an artificial satellite

申请号: US469659

申请日: 1983-02-25

公开（公告）号: US4483570A

公开（公告）日: 1984-11-20

发明人: Masao Inoue

A magnetic bearing arrangement for rotor for controlling the attitude of an artificial satellite wherein the rotor has a rotating speed and an axis of rotation which are adjusted in accordance with a change in the attitude of the satellite. The arrangement includes a stator defined by at least three segments, and each stator segment is provided with a permanent magnet to eliminate the necessity of any electromagnet for controlling radial rotor displacement and any sensor for detecting such radial displacement. The apparatus is free from any eddy currents that may cause great resistance to rotation.

113. MAN-MADE SATELLITE WITH AERODYNAMIC CONTROL VANES

申请号: PCT/FR1994000480

申请日: 1994-04-27

公开（公告）号: WO1994025344A1

公开（公告）日: 1994-11-10

发明人: CENTRE NATIONAL D'ETUDES SPATIALES

Man-made satellite with roll, yaw and pitch control vanes (4, 4', 5) for applying rotational torques to the satellite about its three axes by means of the resistance of the rarefied air surrounding the satellite (dynamic inertia compensation for rotating objects aboard the satellite can also be effected). This invention applies particularly to low orbit satellites.

114. ARTIFICIAL SATELLITE EQUIPMENT PANEL

申请号: US11534684

申请日: 2006-09-25

公开（公告）号: US20070221786A1

公开（公告）日: 2007-09-27

发明人: Hajime TAKEYA; Tsuyoshi OZAKI; Hirotsugu MORINAGA; Shinji BADONO

A satellite equipment panel on which may be mounted an installation equipment of a predetermined function, connectable by an interface, constitutes an artificial satellite. The satellite equipment panel includes a panel body, at least two interfaces for an interconnection to another satellite equipment panel, a line transfer switch disposed within the panel body for line transferring of the interconnection between the interfaces, a wiring disposed within the panel body and connected at one end to one of the interfaces and at the other end to the line transfer switch for interconnecting the interfaces on that panel body. The interfaces and the wiring, in cooperation with a support structure, constitute a wiring module disposed within the panel body. The interface may comprise at least one of interfaces of electric communication, optical communication, and optical sensor.

115. Maneuver device for artificial satellite

申请号: US10078109

申请日: 2002-02-20

公开（公告）号: US06622969B2

公开（公告）日: 2003-09-23

发明人: Toshiaki Yamashita

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.

116. Weather modification by artificial satellites

申请号: US69655

申请日: 1998-04-28

公开（公告）号: US5984239A

公开（公告）日: 1999-11-16

发明人: Franklin Y. K. Chen

A Satellite Weather Modification System (SWMS) uses earth satellites to harness solar energy to modify the thermodynamics and composition of the earth's atmosphere. SWMS has three subsystems: The first subsystem includes a network of earth satellites called Satellite Engines (SEs) used to reflect solar energy and/or transform solar energy into other forms of energy beams discharged at specified locations. The media at these locations and the media through which the energy beams pass absorb these energies and change them into heat. The second subsystem includes a large network of Remote Sensing Devices (RSDs). These sensors are used to measure local media compositions, dynamic parameters and thermodynamic properties. Sensor measurements are fed back to the third subsystem, which includes a network of Ground Control Stations (GCSs). GCSs provide energy beam guidance by estimating each beam's characteristics and its aim point trajectory as functions of time. Integration of these three subsystems establishes a sensor feedback energy beam guidance and control loop. SWMS's weather modification applications include alteration of precipitation, reclaiming of wasteland, reducing damage by bad weather, and improving environment. Its non-weather related applications include supplying concentrated energy to electricity generating stations (solar, wind and hydro), high latitude greenhouse farms, and solar powered airplanes.

117. Artificial satellite communication system

申请号: US886228

申请日: 1992-05-21

公开（公告）号: US5871181A

公开（公告）日: 1999-02-16

发明人: Jonathan Mass

A communication system including a constellation of a plurality of artificial satellites orbiting the Earth, each artificial satellite having communication apparatus providing communication with the Earth, characterized in that the plurality of artificial satellites are in triply-geosynchronous (TGS) orbits having a period of eight sidereal hours, or twice-triply-geosynchronous (TTGS) orbits having a period of sixteen sidereal hours, which orbits are inclined with respect to the Equator and synchronized with the Earth's rotation such as to exploit the natural spacing of approximately 120.degree. in longitude of the major land masses of Europe, North America and the Far East for communication with the artificial satellites to provide for higher elevation angles in such land masses than in other areas.

118. 人工衛星の自律運用計画システムおよび人工衛星の運用計画装置

申请号: PCT/JP2017/025908

申请日: 2017-07-18

公开（公告）号: WO2018016471A1

公开（公告）日: 2018-01-25

发明人: 西山　岳宏; 北村　憲司

衛星側に衛星側運用パラメータ記憶部２２、運用計画部２３を備え、地上側に地上側運用パラメータ設定部１１、衛星側の運用パラメータ記憶部と同じ運用パラメータを記憶する地上側運用パラメータ記憶部１２、衛星側の運用計画部と同一の機能を有する運用計画推定部１４を備え、地上側運用パラメータ設定部１１において運用計画に用いる運用パラメータを決定し、地上側運用パラメータ記憶部１２と衛星側運用パラメータ記憶部２２に随時アップロードし、地上側の運用計画推測部１４と衛星側の運用計画部２３が同一の運用パラメータに基づいてそれぞれ運用計画を作成する。