Hitachi, Ltd.

Tomy Kogyo Co., Ltd.

Nobuo Hamano

Shigeki Nakamura

Masahiro Ito

Tomiharu Yoshida

Takashi Yabutani

Toshihide Maeda

Masataka Owada

Masahiko Ikeda

Kuniyoshi Tsubouchi

Tsutomu Okusawa

Akira Maeda

Koichi Homma

Shimbu Yamagata

Yusuke Takagi

Kazumi Matsumoto

Yoichi Yoshinaga

Yoshio Kojima

Kenji Mitani

Hideji Kondo

Hiroshi Matsumura

A transmission or communication system, wherein plural individual elliptical orbits are so defined that an individual right ascension of a north-bound node is established with a designated angle. An artificial satellite is travels on a respective ones of the plural individual elliptical orbit and a group of artificial satellites arranged on respective ones of the plural individual elliptical orbits are used so that at least one of the artificial satellites having a communication system is always viewable within a pre-defined range of operational elevational angle in a zenith direction from a service area. The group of artificial satellites are on respective orbits obtained by combining an inclination angle and an eccentricity squared of the individual elliptical orbit so that a right ascension of north-bound node is a designated angle and a time period during which respective ones of the group of artificial satellites is viewable from ground is substantially identical.

Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith

A communication terminal for communicating through an artificial satellite, wherein the artificial satellite is placed into an orbit in which an individual satellite orbits on an elliptical orbit so that at least one of the artificial satellites is always viewable within a pre-defined range of operational elevational angle in a zenith direction from a service area. A group of the artificial satellites are satellites on respective orbits obtained by combining an inclination angle and an eccentricity squared of said elliptical orbit so that a time period during which an artificial satellite is viewable from ground is substantially identical and the communication terminal has a transmitter and receiver for transmitting and receiving a signal through the group of artificial satellites.

Communication system, communication receiving device and communication terminal in the system

A broadcasting or transmitting system using an artificial satellite. The artificial satellite is placed into an orbit in which individual artificial satellites orbit on an elliptical orbit so that at least one of the artificial satellites is always viewable within a pre-defined range of operational elevational angles in a zenith direction from a service area. A group of the artificial satellites are satellites on respective different orbits obtained by combining an inclination angle and an eccentricity squared of said elliptical orbit so that a time period during which one artificial satellite of the group of the artificial satellites is viewable from ground is substantially identical to a time period during which another artificial satellite of the group is viewable from the ground.

An information providing method and apparatus for providing information to a moving body via an artificial satellite. Information for selecting a desired information and position information of the moving body is transmitted, from the moving body. Information is provided to the moving body from the artificial satellite depending upon the position information of the moving body and the desired information, on the basis of information from the moving body.

Satellite, satellite control method and satellite communication system

A system and method for a group of artificial satellites. The artificial satellite is placed into an orbit in which an individual satellite orbits on an elliptical orbit so that at least one of the artificial satellites is always viewable within a pre-defined range of operational elevational angle in a zenith direction from a service area. The group of the artificial satellites are satellites on respective different orbits obtained by combining an inclination angle and an eccentricity squared of the elliptical orbit so that a time period during which one artificial satellite of the group of artificial satellites is viewable from ground is substantially identical to a time period during which another artificial satellite of the group of the artificial satellites is viewable from ground.

In order to establish the communication lines among the movable bodies and/or fixed stations and to configure communication system with a small number of satellites, present method has the steps of determining six orbit-related parameters by using a input conditions including a geographical condition of the service area, a desired service time and the tolerance of an ascending vertical angle within which the satellite can be viewed from the service area, and establishing the satellite communication with one or more satellites, an individual satellite being arranged on the orbits selected and combined among plural elliptical orbits corresponding to the determined six orbit-related parameters on which the satellites stay for a sufficiently long time that they may come successfully into sight in the zenith direction.

A communication system, wherein plural elliptical orbits in which an apogee is located on a specified service area are so defined that an individual right ascension of north-bound node may be established with a designated angle. A satellite is made to travel on an individual elliptical orbit and a group of satellites to be arranged on said elliptical orbits are used so that at least one of artificial satellites having a communication system may be always viewable within a pre-defined range of ascending vertical angle in a zenith direction from the service area.

An earth observation system capable of observing the earth globally and uniformly in a steady observation operation mode while observing a given district on the earth in a high-frequency observation operation mode, as occasion requires, includes a plurality of observation satellites each equipped with an orbit transfer facility, an observation data receiving system, an observation satellite operating ground system, an observation command facility such as anti-disaster task forces, institutes or the like. In the steady observation operation mode for observing globally the earth, M observation satellites are constellated on each of L sun-synchronized quasi-recurrent orbits each having a same altitude and a same inclination (where L and M represents natural numbers). In the high-frequency observation operation mode for observing a particular district on the earth, M satellites are constellated on each of L sun-synchronized recurrent orbits each having a nominal altitude of 561 km and a nominal inclination 97.6 degrees or alternatively a nominal altitude of 888.3 km and a nominal inclination of 98.8 degrees.

Earth observation method, and system and observation satellite, operating ground system and program for the same

A gas-liquid separation method for electroconductive gas-liquid two phase flow and the device therefor wherein electrodes are disposed in the vicinity of inlet and outlet portions of the gas-liquid separation region in the flow passage of electroconductive gas-liquid two phase flow so as to flow an electric current thereto. A magnet is disposed in the gas-liquid separation region of the flow passage so as to generate a magnetic field perpendicular to the current and to generate an electromagnetic force acting along the flow passage wall on the electroconductive liquid by taking advantage of the Flemming's left hand law, thereby separating the electroconductive gas-liquid two phase flow into gas phase and liquid phase. A hydrophobic porous material having water permeability is employed as the flow passage wall in the gas-liquid separation region; the gas-liquid separation region is disposed in a reduced pressure region; and the separated gas phase is effectively removed out of the flow passage.

Gas-liquid separation device for electroconductive gas-liquid two phase

Method of opening and closing a fluid passage comprises the steps of freezing fluid in the fluid passage by first cooling the fluid to a temperature below the freezing point of the fluid to close the fluid passage and after the fluid passage is closed, raising the temperature of the fluid close (or just below) to the freezing point of the fluid, whereby the fluid passage is maintained in a closed state with a small power supply and the responsiveness in opening the fluid passage is enhanced.

Shut off apparatus for a fluid passage, method for controlling the same,

Azimuth compression processing is carried out by the steps of determining Doppler rate time change data a reconstructed scene from orbit data of a sattelite or aircraft, determining azimuth coordinates transformation data of an image after range compression, that is, resampling position designation data, from the Doppler rate time change data, resampling the image after range compression, in the azimuth direction using the azimuth coordinates transformation data, keeping unaltered the Doppler rate of a point image relating to the image after coordinates transformation irrespective to the position in the azimuth direction inside the scene, and thereafter using FFT.

Method of reconstructing synthetic aperture radar image

An electronic stereoscopic viewing device has an electronic signal generator which is coupled electronically to a liquid crystal display screen. The display screen upon receipt of a signal from the signal generator displays first and second views of an image with the first and second images being parallactically displaced with respect to one another. A first optical pathway conducts the first parallactically displaced view to a left eye viewing port and a second optical pathway conducts the second parallactically displaced view to a right eye viewing port. The optical pathways between the display screen and the left and right eye viewing ports are such that the first and second images are conducted to the respective left and right eye viewing ports in a manner maintaining the integrity of each such that the individually parallactically displaced first and second views of the images are received at the respective left and right eye viewing ports without contamination of one by the other.

Electronic stereoscopic viewing device

An electronic tennis game having a display panel with ball segments which are illuminated in different sequences to simulate a tennis ball which can move from one side of the tennis court to the other along different trajectories. Player elements are provided on each side of the display panel at positions which intercept the trajectories, each player element including a body portion and racket segments which can be sequentially illuminated to simulate a tennis player swinging his racket. Corresponding to each player element is a return button. A game operator attempts to ascertain the trajectory of an approaching ball and depress the return button corresponding to a player element positioned to intercept it. If the return button is depressed at the right time, the sequentially illuminated racket segments of the selected player element appear to hit the ball back to the other side of the tennis court.

Electronic tennis game with interactive controls

A toy carrier vehicle having a cargo portion sufficiently large to accommodate a powered toy vehicle of the type having a spring motor which is wound by rolling the toy vehicle across a level surface. Openings are provided above the drive wheels of the carrier vehicle to allow contact with the drive wheels of the powered vehicle contained therein. Cargo depression members are provided on the carrier vehicle to force the enclosed powered vehicle against the drive wheels of the carrier vehicle as the latter is rolled across a level surface. Upon completion of the winding operation the enclosed powered vehicle can be retained within the cargo portion to power the carrier vehicle, or it can be released for independent travel.

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Tokyo, Japan

Nobuo Hamano