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63results about How to "Improve position measurement accuracy" patented technology

Non-cooperative target relative navigation motion estimation method and system based on multi-source information fusion

The invention relates to a non-cooperative target relative navigation motion estimation method and system based on multi-source information fusion. The method comprises the following steps of: givinga joint calibration method of a laser and visual measurement system, obtaining the reprojection information of a laser scanning point cloud in camera coordinate system based on the joint calibration system, respectively acquiring the depth compensation information of the target point and the compensated depth information by using a quadratic interpolation method, realizing information fusion between the laser scanning point cloud and the vision camera image, and finally acquiring the motion estimation of the target on the basis of the fusion information. The method provides a fusion method ofinformation of a vision camera and a laser scanner. The high precision depth information of the laser scanning point cloud can be used to compensate for the poor accuracy of the visual image in the depth direction, meanwhile, the defect of low resolution of laser scanning is avoided and the high precision of laser scanning depth information and high image resolution of visual measurement system are integrated. Meanwhile, the interpolation calculation method of information fusion is a simple algebraic operation, which is easy for engineering realization and application.
Owner:BEIJING INST OF SPACECRAFT SYST ENG

Ground testing system for active vibration abatement of flexible spacecraft

ActiveCN104932509AOvercome the problem of difficult simulation of flexible vibration characteristicsExtended vibration acquisition frequency rangeAttitude controlFloating platformAttitude determination
The invention provides a ground testing system for the active vibration abatement of a flexible spacecraft, which comprises a marble air-floating platform, a flexible spacecraft motion simulator suspending above the marble air-floating platform, a rate gyroscope, a photoelectric type attitude sensor, a vibration measuring system, an attitude control flywheel, an attitude control thruster, an orbit control thruster, a vibration abatement system, a motion simulator control computer, a ground measurement system and a ground console. The rate gyroscope, the photoelectric type attitude sensor, the vibration measuring system, the attitude control flywheel, the attitude control thruster, the orbit control thruster and the vibration abatement system are mounted on the flexible spacecraft motion simulator. The motion simulator control computer is mounted on the flexible spacecraft motion simulator and is electrically connected with the rate gyroscope, the vibration measuring system, the attitude control flywheel, the attitude control thruster, the orbit control thruster and the vibration abatement system. The ground measurement system is arranged on the marble air-floating platform and the flexible spacecraft motion simulator. The ground console is connected with the photoelectric type attitude sensor, the motion simulator control computer and the ground measurement system. According to the technical scheme of the invention, the defect that the flexible vibration characteristics of flexible spacecrafts are hard to simulate can be overcome. Therefore, the attitude determination accuracy of the flexible spacecraft motion simulator can be improved.
Owner:SHANGHAI XINYUE METER FACTORY

Measuring method of airborne single-station passive positioning system on target radiation wavelength

The invention discloses a measuring method of an airborne single-station passive positioning system on a measure target radiation wavelength. The measuring method comprises the following steps: making an airborne single-station passive probing platform do constant motion along a straight line; firstly, using the receiving front end to process received probing signals; then, sending the received probing signals into a digital signal processing unit; sending signal frequency values obtained through regular detection under the control of a synchronous clock into a memory; and calling the latest three frequency values from the memory by the data processing unit in a mode of automatic or manual commands under the triggering effect of the regular synchronous clock to measure the wavelength of the measured signals. The invention can accurately estimate and obtain the wavelength of the measure target radiation signals through the simple frequency measuring technology, and the measuring method can be applied to the execution of long distance positioning measuring tasks. However, an aerial measuring platform which has simple equipment and can not be supported by a ground measuring system can also be applicable to the monitoring management of aerial radio signals.
Owner:CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST

Positioning method and device

The invention provides a positioning method and a positioning device. The positioning device applied to a base station side comprises the following steps: acquiring the positioning measurement information of a terminal; receiving a positioning measurement request triggered by a preset positioning entity, wherein the positioning measurement request contains an indication for positioning and measuring the terminal by virtue of a coverage enhancement grade; and sending positioning measurement information of the terminal to the preset positioning entity according to the positioning measurement request so as to drive the preset positioning entity to position the terminal according to the positioning measurement information. According to the embodiment of the invention, the terminal is roughly positioned by a network side through the coverage enhancement grade and a service cell marker of the terminal, so that the extra expenditure of the terminal caused by the positioning of the terminal in the coverage enhancement grade range is avoided, the complexity of the terminal is reduced, and the power consumption of the terminal is saved; or the terminal is subjected to positioning measurement by the network side through a repeated sending property of the coverage enhancement grade, so that a relatively accurate positioning measurement result is obtained, and the positioning measurement precision is improved.
Owner:DATANG MOBILE COMM EQUIP CO LTD

Unmanned aerial vehicle visual attitude and position calculation method based on image marking

The invention discloses an unmanned aerial vehicle visual attitude and position resolving method based on image marking. The unmanned aerial vehicle visual attitude and position resolving method comprises the steps of collecting an aerial image video stream of an unmanned aerial vehicle, extracting a region of interest from an image, extracting angular point coordinates from the region of interest, solving a homography matrix, and solving a relative position and a relative attitude angle of the unmanned aerial vehicle based on an imaging principle. The problem of relatively long time of globally carrying out corner detection is considered, therefore, the retrieval circular ring area is used for carrying out angular point detection on the area in the circular ring; in this way, the calculation amount can be reduced, the operation time can be shortened, the real-time performance of pose determination can be improved, interference of miscellaneous points outside a circular ring can be avoided, the anti-interference capacity can be improved, meanwhile, the three rectangles are adopted, target angular points can be efficiently extracted, and the angular points can be conveniently markedand matched. According to the method, high course measurement precision and high position measurement precision can be kept for a long time, and the method is suitable for application occasions withhigh requirements for the relative position and attitude precision of the unmanned aerial vehicle when two moving carriers such as a landing carrier converge.
Owner:BEIHANG UNIV

Manufacturing method of integral linear motion positioning system based on grating measuring technology

The invention discloses a manufacturing method of an integral linear motion positioning system based on a grating measuring technology. The method comprises the following steps: manufacturing of grating lines on a linear motion component: grinding and polishing the surface of the linear motion component, and then making a grating line structure on the surface of the linear motion component; coating of a grating line protection film: coating the surfaces of the grating lines with a layer of SiO2 protective film; manufacturing of a compact reflective grating reading head: composing a photoelectric conversion part with an LED (Light-Emitting Diode) light source and a grating sensor, and then composing a complete compact reflective grating reading head by a subdivision circuit part; assembling the grating reading head. When the integral linear motion positioning system disclosed by the invention is applied to a numerically-controlled machine tool and a measuring instrument, complex debugging loops during installation of the grating can be omitted, an Abbe error can be avoided effectively, measuring uncertainty is lowered, and the positioning and measuring accuracy of equipment is increased; the method has a wide market prospect and a high popularization and application value.
Owner:CHANGZHOU RUIFENGTE TECH CO LTD

Flexible robot arm shape measuring method and system based on equivalent center point recognition

The invention relates to a flexible robot arm shape measuring method and system based on equivalent center point recognition. The flexible robot arm shape measuring method mainly comprises the steps of acquiring complete side images of arm sections of a flexible robot through a binocular camera fixed on a rigid robot; according to the arm sections respectively detected in the binocular images acquired by the binocular camera, identifying and fitting the contour of an arm lever, and solving image pixel coordinates of the centers of the corresponding arm sections; according to trigger information of man-machine interaction equipment, determining corresponding center points of the same arm section in the left and right ocular images; resolving the pose of the center of the arm lever corresponding to the pixel coordinates of the two center points of the binocular images in the coordinate system of the binocular camera; and through a kinematics algorithm, determining the current pose of the binocular camera relative to a rigid mechanical arm base, and according to the installation position relation of a rigid mechanical arm relative to the flexible robot, converting the solved pose into the pose of the center of the arm lever in the arm section in a flexible robot base coordinate system.
Owner:HARBIN INST OF TECH SHENZHEN GRADUATE SCHOOL

Method and system for autonomous landing of UAV based on photoelectric-inertial combined guidance

In order to overcome defects existing in the existing unmanned aerial vehicle autonomous ship landing technology, the invention provides an unmanned aerial vehicle autonomous ship landing method and system based on photoelectric-inertial combined guidance. According to the method, a coordinate system of a hull-carried inertial navigation system is used as a global reference coordinate system (benchmark), the position and velocity of an unmanned aerial vehicle relative to a hull are acquired through photoelectric tracking systems on the hull, the position and velocity of a ship relative to a local geographic coordinate system are acquired through the hull-carried inertial navigation system, the position and velocity of the unmanned aerial vehicle relative to the local geographic coordinatesystem are obtained through unmanned aerial vehicle strapdown inertial navigation measurement, and the position and velocity information is transmitted to an unmanned aerial vehicle Kalman filter forcombined navigation. In this way, regardless of a satellite signal outside, the unmanned aerial vehicle can perform photoelectric-INS combined navigation, so that the unmanned aerial vehicle gets ridof dependence on an external GPS or Beidou signal in the ship landing process.
Owner:XI'AN INST OF OPTICS & FINE MECHANICS - CHINESE ACAD OF SCI +1

Workbench equipment and method for measuring vertical zero clearing error of workbench

The invention discloses workbench equipment and a method for measuring vertical zero clearing error of a workbench. The workbench equipment comprises a projection objective lens, a main substrate, a workbench, a controller and at least two vertical measuring devices. Each vertical measuring device comprises a light emitter and a light receiver which are correspondingly arranged, and is arranged onone side, close to the workbench, of the main substrate; in a plane perpendicular to the main substrate, the light emitter and the light receiver which are correspondingly arranged are both arrangedon the same side of the immersion head of the projection objective; the light receivers receive measurement light emitted by the corresponding light emitters and reflected by the first measurement point or the second measurement point on the workbench; and the controller obtains the vertical zero clearing error of the workbench according to the vertical heights of the first measuring point and thesecond measuring point. The invention provides the workbench equipment and the method for measuring the vertical zero clearing error of the workbench, and aims to solve the problem that one set of interferometer system cannot cover the whole stroke of the workbench when the vertical zero clearing error is measured.
Owner:SHANGHAI MICRO ELECTRONICS EQUIP (GRP) CO LTD

Rotary transformer

The invention provides a rotary transformer. The rotary transformer includes a stator, and the stator comprises a stator core, an input winding and an output winding, wherein the input winding and theoutput winding are wound on the stator core; the inner side wall of the stator core is provided with a plurality of stator grooves, and the stator grooves are distributed in the circumferential direction, and the two end faces of the stator core are enabled to be connected, so that stator teeth are formed between any two adjacent stator grooves, so as to perform the winding of the input winding and the output winding respectively. The rotary transformer also comprises a rotor, wherein the rotor includes a rotor core. An air gap is defined between the inner side wall of the stator iron core and the outer side wall of the rotor iron core; when the rotor rotates, the length delta of the air gap and the mechanical rotation angle theta of the rotor meet the sine function relation containing the third harmonic component in the circumferential direction, and periodic change is executed according to the function relation so as to define the appearance of the rotor iron core. According to thetechnical scheme, under the condition of the same maximum air gap and the same minimum air gap, the output signal amplitude and the position measurement precision of the rotary transformer can be improved.
Owner:GUANGDONG WELLING AUTO PARTS CO LTD

Rod position measuring method and device based on motion characteristics of control rod of nuclear power station and medium

The invention discloses a rod position measuring method and device based on nuclear power station control rod motion characteristics and a medium, relates to the field of nuclear power stations, and solves the problem that an existing control rod measuring device has an upper limit in measuring precision. An excitation power supply supplies power to a rod position detector; acquiring a measurementsignal from the rod position detector, including acquiring an induced voltage signal of a coil in the rod position detector; separating a fixed frequency signal and a low frequency disturbance signalin the measurement signal, and performing data processing by combining the fixed frequency signal and the low frequency disturbance signal to obtain the position information of the rod position detector and the position information of the control rod bundle. On the basis of not changing the existing structure of the rod position detector, the precision of nuclear power station control rod position measurement can be provided. The effect of the method can be achieved only by changing a signal processing method and increasing low-frequency interference signal processing caused by control rod movement.
Owner:NUCLEAR POWER INSTITUTE OF CHINA
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