Abstract:
A satellite broadcast communications system, in which a host station sends packet-multiplexed signals to a plurality of terminal stations via a communications satellite, specifically improving efficiency in data retransmission operations without sacrificing the channel capacity of the satellite communications link. Broadcast schedule transmission means transmits the broadcast schedule, which contains the title and transmission time of each transmission data, to every terminal station via the communications satellite. Based on the broadcast schedule, composite information transmission means broadcasts various data to the terminal stations. Broadcast schedule reception means receives the broadcast schedule, and based on the received broadcast schedule, desired information reception means selectively receives desired information at the scheduled transmission time. Further, vacant time slot detection means examines the broadcast schedule to find vacant time slots in which no transmission is scheduled, and broadcast schedule production means rearranges the broadcast schedule so that the data once transmitted be retransmitted in those vacant time slots.
Abstract:
The periphery of a disk having flexibility is fixed to a sensor casing, and a force applied to the central portion is detected. A doughnut disk-shaped piezoelectric element is positioned on the upper surface of the disk, and upper electrode layers indicated by patterns of D1 to D6 are formed on the upper surface of the piezoelectric element. Further, lower electrode layers similarly having pattern of D1 to D6 are formed on the lower surface of the piezoelectric element, and the lower surface of the lower electrode layer is fixed on the upper surface of the disk. Six detection elements D1 to D6 are formed each of which is constituted by a of upper and lower electrode layers and a portion of piezoelectric element put therebetween. Thus, force components exerted at an origin defined in the central portion of the disk in respective axes directions of X, Y, Z can be detected based on charges produced in detection elements D1, D2, detection elements D3, D4, and detection elements D5, D6, respectively.
Abstract:
An angular velocity sensor has a flexible substrate and an opposed, fixed substrate supported at their peripheries by a sensor casing. An oscillator is fixed on the lower surface of the flexible substrate. Five lower electrodes are formed on the upper surface of the flexible substrate. Five upper electrodes are formed on the lower surface of the fixed substrate so as to oppose the lower electrodes. For sensing an angular velocity about the X-axis, an a.c. voltage is applied across a predetermined pair of the opposed electrodes to cause the oscillator to oscillate in the Z-axis direction, whereby a Coriolis force proportional to the angular velocity is applied to the oscillator to displace it in the Y-axis direction. As a result, the distance between the opposed electrodes in the positive Y-axis direction becomes smaller, and the distance between the opposed electrodes in the negative Y-axis direction becomes greater, which changes their capacitances to detect the Coriolis force and, thereby, determine angular velocity. It is similarly possible to detect angular velocities about the Y-axis and the Z-axis.
Abstract:
On the upper surface of a flexible substrate, four displacement electrodes are arranged. A fixed substrate is arranged thereabove, and fixed electrodes opposite to the displacement electrodes are respectively arranged on the fixed substrate. These displacement electrodes and the fixed electrodes form capacitance elements C1 to C4, respectively. A columnar working body is fixed on the lower surface of the flexible substrate. A bending is produced in the flexible substrate on the basis of an acceleration exerted thereon. As a result, capacitance values of the respective capacitance elements C1 to C4 vary. The capacitance values of the capacitance elements C1 to C4 are converted to respective voltage values V1 to V4. A component in the X-axis direction is obtained as Vx=(V1+V4)-(V2+V3), a component in the Y-axis direction is obtained as Vy=(V1+V2)-(V3+V4), and a component in the Z-axis direction is obtained as Vz=V1+V2+V+V4.
Abstract:
A sensor for force, acceleration or magnetism is provided which can carries out high accuracy detection without temperature compensation and easily manufactured. The peripheral portion of a disk-shaped substrate (10) having flexibility is fixed to a sensor casing (60), and a working body (50) is connected to the center portion. With respect to the origin (O) within the substrate (10), an X, Y and Z three-dimensional coordinate system is defined, and four sets of detection elements (D1 to D4) are arranged. Respective detection elements are of a sandwich structure in which piezoelectric elements (21, 23) are put between upper electrodes (31 to 34) and lower electrodes (41 to 44). When a force Fx in the X-axis direction is applied to the working body (50) by application of an acceleration, the substrate (10) is bent, so positive or negative charges are produced in respective electrodes. How charges are produced depends upon the direction of an applied force, and a quantity of charges produced depends upon the magnitude of the applied force. Thus, it is possible to detect components in respective axial directions of an applied force on the basis of a pattern of charges produced.
Abstract:
On the upper surface of a flexible substrate, four displacement electrodes are arranged. A fixed substrate is arranged thereabove, and fixed electrodes opposite to the displacement elctrodes are respectively arranged on the fixed substrate. These displacement electrodes and the fixed electrodes form capacitance elements C1 to C4, respectively. A columnar working body is fixed on the lower surface of the flexible substrate. A bending is produced in the flexible substrate on the basis of an acceleration exerted thereon. As a result, capacitance values of the respective capacitance elements C1 to C4 vary. The capacitance values of the capacitance elements C1 to C4 are converted to respective voltage values V1 to V4. A component in the X-axis direction is obtained as Vx=(V1+V4)-(V2+V3), a component in the Y-axis direction is obtained as Vy=(V1+V2)-(V3+V4), and a component in the Z-axis direction is obtained as Vz=V1+V2+V3+V4.
Abstract:
There is disclosed an applied technology of an elementary sensor for sensing a force comprising a transducer for transforming a mechanical deformation to an electric signal, and a first strain generative body (20) including a supporting portion (21) and a working portion (23) connected to the transducer so as to allow the transducer to produce a mechanical deformation on the basis of a displacement relative to the supporting portion of the working portion. By further adding a second strain generative body (30) including a fixed portion (31) fixed at least with respect to the direction of a force to be detected, and a displacement portion (33) connected to the working portion of the first strain generative body, wherein the displacement portion is constructed to produce a displacement based on a given external force relative to the fixed portion to transmit the displacement thus produced to the working portion of the first strain generative body, a force detector applicable to a wide variety of measurement ranges can be realized. Moreover, by allowing the displacement portion to be elongated, a detector suitable for measurement of both force and moment can be provided. In addition, an embodiment to connect stylus (306) to the elementary sensor to apply it to a contact detector, and an embodiment to affix the elementary sensor at the hand of a robot to apply it to a gripper for robot are disclosed.
Abstract:
A force detector is comprised of resistance elements having a piezo resistance effect such that electric resistance varies due to mechanical deformation, and formed on a single crystal substrate (10), and a strain generative body (20) having a supporting portion (21) and a working portion (23), thus allowing the resistance elements to produce a mechanical deformation on the basis of a displacement with respect to the supporting portion of the working portion. This force detector can detect a force applied to the working portion as changes in resistance values of the resistance elements. The plane on which resistance elements are to be formed on the single crystal substrate is selected so that piezo resistance coefficients in two directions perpendicular to each other exhibit peak. When a weight body (30) is connected to the working portion, it is possible to detect an acceleration acting on the weight body. Moreover, when a magnetic body (330) is connected to be working portion, it is possible to detect a magnetic force acting on the magnetic body. By using the detector system for acceleration in common to the detector system for magnetic force to perform a compensation computation, detection of a magnetic force which is not influenced by acceleration can be made. By devising an arrangement of resistance elements in either detector, it is possible to independently determine magnitudes of objects to be measured with respect to directions of the three-dimensional coordinate system, respectively.