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53 results about "Satellite" patented technology

In the context of spaceflight, a satellite is an object that has been intentionally placed into orbit. These objects are called artificial satellites to distinguish them from natural satellites such as Earth's Moon.

Block-based encoding and decoding information transference system and method

InactiveUS7319862B1Power distribution line transmissionSpecial service for subscribersMobile telephonySatellite
Methods, apparatuses, and systems enabling an information exchange system allowing for the transmission of a message carrier containing at least one message code along with video and television data, as well as subsequent capture and decoding of the message carrier to identify the at least one message code. As discussed herein, implementations of the invention can be used in connection with an electronic commerce and data interchange system featuring a Universal Digital Assistant (UDA) that facilitates financial transactions and data interchange, as well as dissemination, management and exchange of commercial information (e.g., advertising, promotions, sales announcements, and the like) and personal information (e.g., address and other contact information, driver's license number, and memberships). The invention, in one implementation, provides an end-to-end e-commerce solution that can transform a mobile phone/PDA (Personal Digital Assistant) into a Universal Digital Assistant configured to receive data (e.g., advertising, promotions, and sales announcement information) based on message codes encoded into message carriers disseminated through advertising and content from analog and digital television broadcasts, television receivers, the Internet, wireless signals, radio broadcasts, satellite broadcasts, and print media.
Owner:EXPHAND

Intelligent rainwater system based on runoff simulation and multi-sensor monitoring, and operation method

PendingCN109164509ACompensating for lagging solid-state rainfall monitoringMaster water absorption capacityIndication of weather conditions using multiple variablesICT adaptationMeasuring instrumentRadar rainfall
The invention discloses an intelligent rainwater system based on runoff simulation and multi-sensor monitoring, and an operation method. The system comprises a runoff simulation and control host basedon a GIS, a meteorological forecast and runoff satellite monitoring server, a distributed small meteorological station, a vertical surface rain condition monitor, a movable rainfall radar, an infrared video monitor, an evaporation measuring instrument, a rainwater pipe network flow monitor, a water quality online monitor, an air quality monitor, a radar rainfall monitor, an infiltration area saturation monitor, an accumulation area water level monitor, a shallow-layer underground water level monitor, a surface runoff monitor, a waterproof unmanned aerial vehicle with a speed measuring buoy, an optical fiber temperature sensing system, an optical fiber pressure sensing system, a communication module, an intelligent controller, a rainwater utilization facility water supply point, a high-position rainwater hydroelectric generation module, a submersible conveying pump, a pressurization infiltration device and the like. According to various parameters, the rainfall flood disasters are subjected to scientific early warning and warning, and measures are adopted, so that the disaster risk of rainfall flood disasters to a building area or a building can be reduced.
Owner:CHINA RAILWAY CONSTR GROUP

Flat plate reflective array antenna

ActiveCN101814660ASimplify the design processImprove the envelopeRadiating element housingsMicrowaveDielectric plate
The invention relates to a flat plate reflective array antenna which comprises the following components: a metallic bottom plate, a dielectric plate, a polarized grid plate, wave absorbing material surrounding edges, an antenna cover and a feed source, wherein the dielectric plate is installed on the top of the metallic bottom plate and is parallel with the metallic bottom plate; the polarized grid plate is supported on the dielectric plate through a supporting pillar, is parallel with the dielectric plate and the metallic bottom plate, and has a certain distance to the dielectric plate and the metallic bottom plate; the wave absorbing material surrounding edges are installed at the periphery of the metallic bottom plate so as to surround the dielectric plate and the polarized grid plate;the antenna cover is buckled with the metallic bottom plate so as to surround the dielectric plate, the polarized grid plate and the wave absorbing material surrounding edges; and the feed source is installed at the center of the bottom of the metallic bottom plate and passes through the metallic bottom plate and the dielectric plate. The antenna has the advantages of simple feeding, high gain, good directional diagram envelope, wide frequency band, small volume, light weight, easy installation and the like, and can be used for the fields of microwave communication, satellite communication and the like.
Owner:COMBA TELECOM SYST (GUANGZHOU) LTD +1

Adaptive focusing system and focusing method for fast imaging of spatial optical camera

InactiveCN105629629AEnsure fast, high-quality imaging of issuesJudgment to solve out-of-focusMountingsFocusing aidsRapid imagingCamera control
The invention relates to an adaptive focusing system and focusing method for fast imaging of a spatial optical camera. The adaptive focusing system comprises a main reflector temperature collection unit, a camera controller unit and a focusing mechanism unit, wherein the camera controller unit is connected with the main reflector temperature collection unit and the focusing mechanism unit. The adaptive focusing system solves the problem of out-of-focus judgment on a temperature change caused by a coaxial three-mirror carbon fiber optical system of the spatial optical camera, omits the processes of artificial out-of-focus judgment of downloaded data, out-of-focus amount calculation, focusing instruction injection and the like, achieves real-time closed-loop adjustment of a focal plane of the optical system of the camera and the camera temperature, solves the fast high-quality imaging problem under the condition of an unbalanced temperature after the spatial optical camera enters an orbit, and provides a technical support for fast imaging development of a spatial optical satellite of our country.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

Embedded Internet of things gateway-based agricultural greenhouse indoor environment monitoring system

ActiveCN105610900AEasy to monitorEffective monitoringTransmissionSimultaneous control of multiple variablesIot gatewayWeb service
The invention relates to an embedded Internet of things gateway-based agricultural greenhouse indoor environment monitoring system. The system is characterized in that the system includes a user end, a web server, an embedded type Internet of things gateway, a plurality of environmental parameter sensors, a plurality of execution devices, a database and a power supply device; the environmental parameter sensors are arranged in an agricultural greenhouse and are used for transmitting acquired environmental parameters in the agricultural greenhouse to the embedded type Internet of things gateway through a bus control local area network or a wireless local area network; the embedded type Internet of things gateway sends received environmental parameter data to the web server through the Internet or other satellite networks; the web server processes received data and sends control instructions to the embedded type Internet of things gateway; the embedded type Internet of things gateway sends the control instructions to the execution devices in the agricultural greenhouse through the wireless local area network or the bus control local area network, so that the execution devices can act; and the power supply device is used for supplying power for all electric devices.
Owner:FRUIT TREE INST OF CHINESE ACAD OF AGRI SCI +1

Satellite ground micro-vibration test system

The invention discloses a satellite ground micro-vibration test system. The satellite ground micro-vibration test system comprises a high-sensitivity sensor used for extracting vibration signals near a disturbance source or a load, an anti-aliasing filter used for performing anti-aliasing filtering on the vibration signals extracted by the high-sensitivity sensor to form piezoelectric signals, a high-modulus conversion rate acquirer used for generating the piezoelectric signals into digital signals and a high-precision controller used for controlling display, storage and analysis of the digital signals. According to the invention, the high-sensitivity sensor realizes small-magnitude acquisition of the vibration signals, digital signals are generated through a high-precision data acquisition card after the vibration signals are subjected to the anti-aliasing filtering, and subsequent process is performed to provide efficient input for the subsequent satellite vibration reduction or vibration isolation and environmental test and also realize verification of vibration reduction or vibration isolation performance. Therefore, the satellite ground micro-vibration test system, disclosed by the invention, has the advantages of satisfying demands on acquisition and analysis of micro-vibration signals and being of great importance in improving control precision and stability of a satellite platform.
Owner:SHANGHAI SATELLITE ENG INST

Starting method of satellite borne software

InactiveCN106648809AImprove securitySave space costProgram loading/initiatingStatic random-access memoryProgrammable read-only memory
The invention relates to a starting method of satellite borne software. The method comprises the following steps: ground compression software stores an object code of the satellite borne software in a programmable read only memory (PROM) after multiple lossless compression; and after a satellite computer is electrified or reset, a starting program decompresses and reduces compression data of the satellite borne software stored in the PROM to a static random access memory (SRAM) and operates. The memory efficiency of the PROm is effectively improved, the flight program and the starting program which are normally cured in the PROM are realized, so that the space cost and the maintenance cost brought by redundant backup are lowered, the safety of the satellite is extremely improved, the PROM is not overturned by single particles, EEPROM is not dependent, on-orbit maintenance times in the later stage can be greatly reduced, and the fault-tolerant ability of operation of the satellite borne computer is enhanced.
Owner:SHANGHAI AEROSPACE CONTROL TECH INST

Monitoring system for electric vehicle

InactiveCN101276516AImprove protectionVehicle testingDetection of traffic movementIntegrated Services Digital NetworkEngineering
The invention provides an electric vehicle monitoring system in which an electric vehicle (A) is equipped with a control device (4) for detecting vehicle state information such as position information, speed, incline situation, etc., of the electric vehicle (A) from an orbiting satellite according to GPS and storing the information, the control device can notify a monitoring center (B) according to sending of the electric vehicle (A), that is data communication or audio communication, and via a network (8) such as an integrated services digital network (ISDN) or the like used as a base station or a switch network. Further, the monitoring center (B) transmits the information to a client terminal (C) such as a contract party or the like via the network (8), the client terminal (C) recognizes the information by a terminal information device, such as a personal computer, a fixed telephone, other mobile phones, etc., for example, the monitoring system of the electric vehicle can treat accidents of the electric vehicle (A).
Owner:时实贵美子

Detection method and detection system for detecting infrared weak and small target

ActiveCN107256560AImprove robustnessReduce distractionsImage enhancementImage analysisFalse alarmLightness
The invention provides a detection method for detecting an infrared weak and small target. The method comprises the steps of background suppression: suppressing the background of a target by utilizing brightness contrast significance-based radiation energy characteristics and the isotropic characteristics of a fan-shaped Gaussian differential filter; track extraction: extracting the movement track characteristics of the target by utilizing an inter-frame difference method and a constant false alarm rate threshold value segmentation method; and result output: according to the movement track continuity of the track, obtaining a final detection result. The invention further provides a detection system for detecting the infrared weak and small target. Based on the technical scheme of the invention, the directional characteristics, the energy characteristics and the movement characteristics of the ground observation image of a sky-based satellite are comprehensively analyzed. Therefore, the interference on various complex false alarm sources on the ground surface is effectively weakened. The false alarm rate of the detection is reduced, and the robustness of the algorithm is enhanced. Moreover, the calculation is simple and efficient, and the real-time performance is high. The method and the system can be conveniently realized on a hardware platform.
Owner:BEIJING INST OF ENVIRONMENTAL FEATURES

Satellite task planning method for realizing maximum observation area by limited coverage resource

ActiveCN110727903AExcellent Arrangement ResultsOptimal feasible solutionForecastingComplex mathematical operationsInteger linear programming modelDistributed computing
The invention discloses a satellite task planning method for realizing maximum observation area by limited coverage resources, which comprises the following steps: 1, discretizing and expressing an area to be observed by using grids, so that the original coverage problem of a larger area is converted into the coverage problem of the grids; 2, establishing an integer linear programming model of theproblem based on the grid, and designing a heuristic algorithm based on dynamic greedy by taking the realization of the maximum coverage area as an optimization target; 3, repeatedly refining the grid in a nested manner, and proposing a method for constructing an adjacent coverage mode on the new grid to prevent all coverage modes from being regenerated each time; and 4, combining grid refinement, construction of a near coverage mode and a dynamic greedy-based heuristic algorithm, and performing multiple iterations to obtain a better feasible solution. According to the method, the satellite task arrangement result with the maximum coverage area as the purpose can be quickly obtained, so that the satellite can fully utilize limited observation resources to complete observation tasks as many as possible, and the utilization efficiency of satellite resources is improved.
Owner:HEFEI UNIV OF TECH

Distance measurement method for automatically eliminating dynamic distance zero value

The invention provides a distance measurement method for automatically eliminating a dynamic distance zero value. According to the distance measurement method, operation is easy, convenient and reliable, measurement is accurate, the single processing and information processing way is not limited, and the distance zero value caused by signal processing time delay does not need to be calibrated. According to the technical scheme, the method comprises the steps that at first, a satellite-borne terminal achieves downlink signal processing, at the moment, the measurement value for uplink signals is collected and stored, and the current measurement value is inserted into the next frame of downlink data to execute signal processing related steps; then, a ground terminal receives the downlink information, meanwhile collects the measurement value of the uplink signals and sends the measurement value to a computing terminal, measurement information in a data frame is obtained to be sent to the computing terminal, and the computing terminal obtains a satellite-ground two-way distance measurement value by comparing the measurement value collected by the ground terminal with the measurement information obtained in the next frame of data. According to the distance measurement method for automatically eliminating the dynamic distance zero value, restrictions of an existing method to signal processing and information processing way are thoroughly eliminated, and signal processing and information processing do need to be calibrated.
Owner:10TH RES INST OF CETC

Method for realizing light-weight high-accuracy composite material frame

ActiveCN102145752AReduce structural weightSmall thermal deformationCosmonautic vehiclesCosmonautic partsJoint spacerMaterials science
The invention relates to composite material frames for spacecrafts such as satellites and the like. The problem to be solved is to provide a method for realizing a light-weight high-accuracy composite material frame, and the high-accuracy requirement on the installation of effective loads is met through processes. The device is characterized by mainly comprising rectangle cross section rod pieces[1], joints [2], joint spacers [3], joint bushing blocks [4] and rod built-in pieces [5] which are made of composite materials, wherein a frame main body consists of a certain number of rectangle cross section rod pieces [1] and joints [2] in the integral structure; the rod built-in pieces [5] are hinged in the rectangle cross section rod pieces [1]; the joint spacers [3] are hinged on the outer surfaces of the joints [2]; and the joint bushing blocks [4] are hinged inside the joints [2]. By the method, the problems of installation and supporting between the effective loads and bodies of the spacecrafts such as the satellites and the like are solved, the installation accuracy of the effective loads is effectively ensured, and the local rigidity requirement on the installation of the effective loads is met simultaneously; and the method has good effects of ensuring the machining stability of the integral structure and improving the applicability and the reliability of the structure.
Owner:SHANGHAI SATELLITE ENG INST

Integrated platform supporting hinge

ActiveCN110906116AConformationally stableImprove support stiffnessStands/trestlesPhysicsSatellite
The invention provides an integrated platform supporting hinge, which comprises an integrated connecting rod, a magnetometer, an attitude measuring instrument, a Y-shaped supporting flexible hinge, asupporting platform and an I-shaped supporting flexible hinge. The magnetometer and the attitude measuring instrument are arranged at two ends of the integrated connecting rod respectively; and the integrated connecting rod is connected to the supporting platform in a supporting mode through the Y-shaped supporting flexible hinge and the I-shaped supporting flexible hinge. Through thermodynamic decoupling of the Y-shaped supporting flexible hinge and the I-shaped supporting flexible hinge in two dimensions and high rigidity in the vertical direction, no-thermal stress support of the Y-shaped supporting flexible hinge and the I-shaped supporting flexible hinge and constancy of the positions of key components of the magnetometer are realized, thereby facilitating scientific tests and applications in satellite fields such as space magnetic field and gravitational field detection. The integrated platform supporting hinge has the advantages of no thermal stress support, constant key component pose, stable platform configuration, high support rigidity, reliable performance and simple structure and the like.
Owner:SHANGHAI SATELLITE ENG INST
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