52 results about "Full moon" patented technology

The invention discloses a method for manufacturing a digital elevation model by using data of a laser altimeter. The method comprises the following steps of: acquiring elevation measurement data by using the laser altimeter; filtering the elevation measurement data of the laser altimeter; and filtering, and interpolating the laser elevation measurement data subjected to singular point removal, and manufacturing the digital elevation model (DEM) with full moon regular grids. Because full moon data is used, the data accuracy and the resolution of the moon DEM manufactured by using the method are obviously increased by using the filtering and interpolating process.

The invention discloses a method for accurate focal length measurement of an optical imaging system based on moon imaging. The method for accurate focal length measurement of the optical imaging system based on moon imaging comprises the steps that a moon image is obtained through the optical imaging system, the edge of the moon image is extracted based on the sub pixel edge detection algorithm, primary fitting is conducted by means of extracted edge information to enable a primary rough fitting disc to be obtained, fitting is conducted on the moon disc with the least square method and progressive optimization is conducted based on distance constraint to enable a high-precision sub-pixel-level moon disc to be obtained, and the focal length of the optical imaging system is calculated by means of the relative position geometrical relationship. Compared with the prior art, the method for accurate focal length measurement of the optical imaging system based on moon imaging has the advantages that the problems that during ground development, the measurement cost of a large-focal-length optical imaging system is high, a measurement device is complicated, the difficulty of focal length measurement of the optical imaging system is high during in-orbit operation, and the precision is limited are solved, the moon is fully used for imaging, the diameter of the moon disc is obtained through sub pixel extraction with the least square method, both a 'full moon' and a 'waning moon' can be used for focal length measurement, and the method is an economical and reliable focal length measurement method for large-focal-length optical imaging systems.

The invention discloses a measurement method of energy flux density distribution of heliostat filed of a tower type power station. The method comprises the following steps: (1), computing the positionangles of the sun at day time and the moon at night at different times, and recording times corresponding to the sun and the moon when the position angles of the sun and the moon are the same; (2), selecting day time, full moon night and unclouded full moon night when the position angles of the sun and the moon are the same, arranging an illuminometer array on a heat absorber of a tower type heliostat filed sun tower, and measuring the energy flux density of a concentrating light spot; obtaining the relative energy flux density of a moonlight concentrating light spot, namely a concentrating ratio function by comparing a moonlight normal direct illuminance measured through a moonlight measuring station; measuring a sun normal direct illuminance at a particular time through a sun measuringstation at day time with the same position angle with the unclouded full moon night, multiplying the sun normal direct illuminance with the concentrating ratio function, so as to obtain the energy flux density distribution of the discrete tower type heliostat filed to a sun concentrating light spot, and obtaining the f energy flux density distribution of the continuous sunlight concentrating lightspot through data interpolation.

The invention provides a laser ablation obstacle removing apparatus. The laser ablation obstacle removing apparatus comprises a low-power optical fiber laser, an indicating laser, a high-transmittancehigh reflector, a first full moon scimitar-shaped lens and a second full moon scimitar-shaped lens, wherein the low-power optical fiber laser comprises a laser seed source, an optical fiber pre-amplification stage (a semiconductor laser pumping source, a light beam coupler and first gain dielectric optical fibers) and an optical fiber power amplification stage (a semiconductor laser pumping source, a light beam coupler and second gain dielectric optical fibers). The laser ablation obstacle removing apparatus is hoisted on an unmanned aerial vehicle through a damping bolt, so that foreign matters on a high altitude power transmission line can be removed by ablation in long-distance manner.

The invention provides an amusement facility which is mainly composed of a simulation goddess in the moon, an upper base, a lower base, a slip rope, a simulation moon, a lifting rod, a lifting frame and the like. Through movement of the simulation goddess in the moon on the slip rope, the scene that the goddess in the moon flies to the moon is simulated; light on a lamp panel is grouped according to the projection of a profile plate, the light groups are controlled to be lightened layer by layer through a controller, and the gradual change process of the moon from the new moon to the full moon is formed; the simulation moon image is driven by a motor to rotate on an upper rotating shaft and a lower rotating shaft, and the scene that the goddess in the moon gradually enter the moon from bottom to top is achieved.

The invention discloses a production technology of a luminous silk decorative material applied to building interiors of commercial clubs. The production technology comprises the steps of base paper production, silk processing, adhesion, coating, calendering, luminous coating liquid preparation, spraying and shearing, and through the steps, the luminous silk decorative material which is composed of a base paper layer, a silk layer, a foaming material layer and a luminous coating liquid layer and is applied to the building interiors of the commercial clubs is finally prepared. The production technology of the luminous silk decorative material disclosed by the invention is relatively low in cost as well as simple and convenient in process, and silk fabrics are combined with antibacterial base paper for the first time to improve the interior grade, physical strength and service cycle; the illumination intensity of the building interiors can be greatly increased through the coating of the luminous coating liquid; the advantages of energy conservation and environmental protection can be achieved; and meanwhile, compared with commercial interior materials, the luminous silk decorative material disclosed by the invention has obvious advantages in bursting strength, environmental protection grade, antibacterial and mildew-proof grade, life cycle and full moon luminous intensity.

The invention discloses a geostationary satellite lunar image navigation registration method based on geometric position precise calculation, belongs to the field of positioning and measurement technology, and is used for lunar observation image navigation registration. Data preparation includes preparing satellite attitude data, lunar ephemeris data, lunar image data, satellite position and speed data; data processing includes edge detection, ellipse fitting, obtaining ellipse parameters, image clipping, Gaussian filtering, Gaussian filtering results are fed back to edge detection, ellipse fitting obtains the geometric center of the lunar image, and the ellipse parameters are used to verify the fitting results; model construction includes establishing a conversion matrix between coordinate systems, calculating the scanning angle and step angle of the image center, obtaining the full-moon scanning angle and step angle, using the method of positioning the lunar surface point using the optical axis of the sensor, converting the two angles of the lunar surface point into lunar surface coordinates, and finally outputting the registration results. The invention can successfully realize the conversion of lunar image coordinates to lunar surface coordinates with high accuracy.

The invention discloses a starmoon ceiling-mounted lamp. The lamp comprises a translucent lampshade, a lighting panel, a wireless LED lamp, a controller, a ballast and a remote control unit. The lighting panel is arranged at the center of the translucent lampshade, divided into four valvular partitions and provided with the controller and the ballast. Light emitting of the four valvular partitions is arranged corresponding to the waning moon, the quarter moon, the gibbous moon and the full moon of the phase of the moon. Each partition comprises a light source, a dodging plate and a reflecting surface. The wireless LED lamp is arranged around the lighting lamp. A wireless receiver is arranged at the control end of the controller. The control end of the ballast is connected with the controller, and the output end of the ballast is connected with the four valvular partitions. A control key of the remote control unit comprises a switch control key and a brightness adjusting key of the four valvular partitions and a switch control key of the wireless LED lamp. By the adoption of the mode, different moon shape lighting and starlight decoration lighting combinations are arranged according to requirements, and the starmoon ceiling-mounted lamp is attractive and practical.

1. The name of the design product: charging pile (full moon). 2. The use of the design product: used for monitoring the parking space condition, identifying the license plate number, and linkage control of the ground lock while providing charging service. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: design 1 perspective view 1. 5. Design 1 is designated as the basic design.

1. Name of the product in this design: Sideboard (Full Moon). 2. Purpose of this design: For placing items. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model.

1. Name of the product in this design: Fireworks Fixing Device (Full Moon). 2. Purpose of this design: For fixing cylindrical fireworks. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: 3D view 1.

1. The name of this design product: Chandelier (Flowers and Full Moon). 2. Application of this design product: indoor lighting. 3. The key point of the design of this product lies in its shape. 4. The picture or photo that best illustrates the key points of the design: Design 6 three-dimensional diagram. 5. Designate Design 6 as the base design.

1. Name of the product in this design: Chandelier (Blooming Flowers and Full Moon). 2. Purpose of this design: Indoor lighting. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the key design points: Design 1 3D view. 5. Design 1 is designated as the basic design.

The present invention provides an indirect measurement method for the concentration ratio distribution of a heliostat field in a tower power station by using moonlight, and the steps are as follows: On the night of the concentration experiment, modify the time and date of the heliostat field control system so that the running trajectory of the sun is close to that of the moon on that night, and the heliostat field tracks the moon according to the solar position program to achieve the concentration of the heliostat field on the moon; Conduct a moonlight concentration measurement experiment in the tower heliostat field. During the measurement process, move the white board of the linear array illuminometer up and down to sweep across the receiving surface of the heat absorber, and the linear array illuminometer measures the moonlight concentration illumination distribution; The moonlight normal direct illumination measurement station continuously measures the moonlight normal direct illumination; Calculate the moonlight concentration ratio distribution of the heliostat field on the receiving surface of the heat absorber; Determine the number of times N of repeated mean smoothing filtering according to the ratio of the lunar phase on that night to the full moon; After the moonlight concentration ratio distribution is subjected to N times of repeated mean smoothing filtering, the concentration ratio distribution of the heliostat field for sunlight is obtained.

The invention discloses an agile remote sensing satellite on-orbit autonomous focusing method based on lunar imaging, and the method comprises the following steps: enabling the satellite to carry out attitude maneuver when the lunar phase is a full moon or a convex moon, enabling the satellite to be converted from earth pointing to lunar pointing, enabling the satellite to reach a stable state, and entering a lunar focusing mode; when the agile remote sensing satellite is in the earth shadow area, controlling the load focusing mechanism to adjust the focal plane position, and obtaining lunar images corresponding to the n focal plane positions; the satellite carries out attitude maneuver, and lunar pointing is converted into earth pointing; and the on-satellite data processing subsystem performs on-orbit calculation on the definition of all moon images, and determines the position with the maximum definition value as the optimal focal plane position. The moon images at different focal plane positions are obtained through attitude maneuver, the definition is calculated, the optimal focal plane position is judged, and the problem that an existing on-orbit focusing method depends on human intervention is solved.

1. The name of this design product: Lawn lamp holder (full moon). 2. Purpose of this design product: outdoor lighting. 3. The design key point of this appearance design product lies in the shape. 4. The picture or photo that best illustrates the key points of the design: 3D drawing of Design 1. 5. Designate Design 1 as the base design.

1. Name of the product in this design: Packaging Box (Full Moon). 2. Purpose of this design: For packaging products. 3. The key design features of this product are the combination of shape and pattern. 4. The image or photograph that best illustrates the design's key points: a 3D model.

1. Name of the design product: Medal (Golden Osmanthus and Full Moon Y4493). 2. Use of the design product: Medal or souvenir for awarding prizes. 3. Design key points of the design product: The combination of shape and pattern. 4. Picture or photo that best shows the design key points: Perspective view 1. 5. This design product is a thin product, and the left view, right view, top view, and bottom view are omitted.

1. Name of the product in this design: Fireworks (Blooming Flowers and Full Moon). 2. Purpose of this design: for fireworks displays. 3. The key design features of this product are the combination of shape and pattern. 4. The image or photograph that best illustrates the design's key points: a 3D model.

1. Name of the design product: Stone carving (Happy union of flowers and full moon). 2. Use of the design product: The design product is used for decoration and ornaments. 3. Design key points of the design product: It lies in the combination of shape and pattern. 4. Picture or photo that best shows the design key points: Three-dimensional view.