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177 results about "Constant angular velocity" patented technology

In optical storage, constant angular velocity (CAV) is a qualifier for the rated speed of any disc containing information, and may also be applied to the writing speed of recordable discs. A drive or disc operating in CAV mode maintains a constant angular velocity, contrasted with a constant linear velocity (CLV).

Magnetic data storage fixed hard disk drive using stationary microhead array chips in place of flying-heads and rotary voice-coil actuators

A magnetic data storage fixed hard disk drive using stationary Microhead Array Chips in place of conventional Flying-Heads and Rotary Voice-Coil Actuators or other Servo-Tracking mechanisms. Every Microhead Array Chip has a minimum of one thousand or maximum of four billion individual and addressable microhead read and write data-transducers built into it. The hard disk drive unit assembly that uses the Microhead Array Chip approach will have within its assembly as few as two or as many as twenty-eight installed Microhead Array Chips. The Microhead Array Chip hard disk drive unit assemblies will have at least one storage disk-platter with two disk-platter data-surfaces containing a multiplicity of concentric data-tracks that rotates at a substantially constant angular velocity. While Microhead Array Chips are made stationary by specially designed circuit boards, that positions a Microhead Array Chip over each of two data-surfaces of every disk-platter within the hard disk drive assembly. The total number of microheads within a stationary positioned Microhead Array Chip's Microhead Array is what determines the total number of available tracks on and across a data-platter's data-surface (i.e., 65,000 microheads would equal 65,000 cylinder/tracks).
Owner:OPTICAL STORAGE DEVICES

Optical data storage fixed hard disk drive using stationary magneto-optical microhead array chips in place of flying-heads and rotary voice-coil actuators

An optical data-storage hard disk drive, which uses stationary Magneto-Optical Microhead Array Chips in place of conventional Flying-Heads, Rotary Voice-Coil Actuators and other similar types of Servo-Tracking mechanisms to transcribe or retrieve digital information to or from at least one non-volatile memory medium's data-surface, using an optical magnetic process of recording and reading data. The Magneto-Optical Microhead Array Chip Hard Disk Drives will have at least one storage disk-platter with two disk-platter data-surfaces containing a multiplicity of concentric data-tracks that rotates at a substantially constant angular velocity. Every Magneto-Optical Microhead Array Chip will comprise a (VCSEL) "Vertical Cavity Surface Emitting Laser" microhead array having a minimum of one thousand or a maximum of four billion individually addressable VCSELs. Each Magneto-Optical Microhead Array Chip is placed into a stationary position above each disk platter data-surface using a chip-positioning circuit board. While the number of cylinder/tracks available to each Magneto-Optical Microhead Array Chip is determined by the number of VCSEL microheads contained within a Magneto-Optical Microhead Array Chip's microhead array (e.g., "325,000" vertical cavity surface emitting laser microheads would therefore equal "325,000" corresponding cylinder/tracks).
Owner:OPTICAL STORAGE DEVICES

Light beam position and polarization angle common light path detection device and method

The invention discloses a light beam position and polarization angle common light path detection device and method based on a photoelectric position sensor. The method comprises the following steps: utilizing a lateral excursion and polarization dispersion prism to shape an incident light beam, outputting orthogonal parallel polarized lights with proportionable light intensities and realizing the contactless space position attitude transfer function; enabling a receiving system to utilize a rotary motor with a coder to drive an analyzer to detect the beacon light polarization through rotation at a constant angular velocity, utilizing the horizontal photoelectric effect of a PSD (Phase-sensitive Detector) to measure the light spot imaging position of beacon light and reversely pushing a beacon light beam position coordinate according to the imaging principle; utilizing light current generated by gathering incident light intensities on the surface of the PSD to detect the incident light intensities, comparing with an angle instantaneously fed back by the rotary motor, obtaining the synchronous polarization angle information of a beacon light beam after the phase sensitive detection, and achieving the function of simultaneously adjusting and detecting the beacon light track and the base vector angle on a same light path and a device. The light beam position and polarization angle common light path detection device has the benefits of simple structure and simple components and is suitable for the multi-dimensional angle measurement demands.
Owner:SHANGHAI INST OF TECHNICAL PHYSICS - CHINESE ACAD OF SCI

Inertial space gyro calibration test method based on three-shaft turntable

The invention relates to an inertial space gyro calibration test method based on a three-shaft turntable; while a gyro assembly attitude rotation is provided by the three-shaft turntable, the compensation dosage of the earth autorotation angular velocity is calculated according to the real-time rotating angle output of three rotating shafts of the three-shaft turntable, so that the influence of earth autorotation on the gyro measurement output is eliminated, and the inertial space constant angular velocity required for a gyro calibration algorithm is ensured. At the same time, based on attached rotation characteristics of the three rotation shafts of the three-shaft turntable, the method defines a rotation sequence rule of the three rotation shafts and a three-shaft turntable body coordinate system and a reference inertial coordinate system having the initial zero coinciding with the ground horizontal coordinate system, and provides a reference benchmark for determining the inertial system angle increment according to the gyro output and for determining the inertial system attitude according to the rotation angle output of the three rotation shafts of the three-shaft turntable. The method can significantly improve the precision of a ground gyro calibration test, can guarantee the ground to perform effective calibration and test result calibration on a gyro assembly, can establish a good foundation for performing relevant calibration tests of satellites in orbit, and improves the determination precision of the gyro attitude.
Owner:BEIJING INST OF CONTROL ENG

Time delay test system and method used for virtual reality helmet acceleration motion

The present invention discloses a time delay test system and method used for virtual reality helmet acceleration motion. The time delay test system used for the virtual reality helmet acceleration motion is characterized in that an arc-shaped scale, a virtual reality helmet and a camera are arranged orderly at intervals along a straight line and are fixedly arranged on a controllable rotating disc, a servo motor is arranged below one side of the controllable rotating disc, and the output shaft of the servo motor is fixedly connected with the controllable rotating disc; a display screen of the virtual reality helmet displays a virtual scale, the servo motor drives the controllable rotating disc to rotate at a constant angular velocity, and the camera shoots the arc-shaped scale and the virtual reality helmet on the controllable rotating disc; the interface of the virtual scale of the display screen of the virtual reality helmet in an image is analyzed to obtain the measurement amount, and further the delay amount of the virtual reality helmet is calculated. According to the present invention, a time delay test of the virtual reality helmet acceleration motion is realized, the total delay of the system is measured accurately, a view angle error brought by shooting can be avoided, the system accuracy is improved, and a final test result is accurate and reliable.
Owner:杭州映墨科技有限公司

Method for modulating angular movement of isolation carrier in inertial navigation system through rotation

The invention discloses a method for modulating angular movement of an isolation carrier in an inertial navigation system through rotation. The method comprises the steps of calculating rotation angular velocity, relative to a navigation coordinate system, of a rotating platform at the k control moment according to the rotating scheme of the rotating platform; controlling the rotating platform to rotate, so that an IMU coordinate system p coincide with a carrier coordinate system b; modulating the inertial navigation system to enter the navigation state through rotation, so that control angular velocity of an inner ring shaft and control angular velocity of an outer ring shaft in the rotating platform within the first control cycle are obtained; predicting movement angular velocity, relative to the navigation coordinate system, of the carrier within the (k+1) control cycle and rotation control angular velocity, relative to the carrier coordinate system, of the rotating platform; obtaining the control angular velocity of inner ring shaft and the control angular velocity of the outer ring shaft in the rotating platform; controlling the control angular velocity of inner ring shaft and the control angular velocity of the outer ring shaft, and eliminating influence of the angular movement of the carrier, so that isolation of angular movement of the carrier is achieved. By means of the method for modulating angular movement of the isolation carrier in the inertial navigation system through rotation, the rotation modulation effect is guaranteed, and precision of the navigation system is improved.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Seat supporting assembly and wheelchair including same

A seat supporting assembly (24) for supporting a seat (18), the assembly comprising a base (25) including a substantially elongated guiding rod (58), a seat support (36), a seat support-to-base linking member (56) pivotally coupled to the seat support (36) and sliding on the base guiding rod (58), a substantially elongated tilting member (60) having a guiding groove (66) and being pivotally attached to the seat support (36) and to the base (25). An actuating assembly (44) is coupled to the base (25) and includes a motion transmitting member (68) mounted within the guiding groove (60). The force from the actuating assembly moves the tilting member (60) according to the geometry of the guiding groove (66), which causes the seat supporting assembly (24) to move between tilted and upright configurations by pivoting the tilting member (60) relative to the seat support (36) and the base (25) and substantially simultaneously moving the seat support-to-base linking member (56) longitudinally relative to the guiding rod (58). The assembly is designed to maintain the location of the center of gravity of a user as the seat tilts rearwardly by automatically moving the seat forwardly during tilting. The guiding groove (66) in the tilting member (60) may be curved such that the tilting motion occurs with a constant angular velocity The seat assembly is particularly useful for wheelchairs.
Owner:AMYLIOR
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