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118 results about "Solar angle" patented technology

Automated shade control method and system

This invention generally relates to automated shade systems that employ one or more algorithms to provide appropriate solar protection from direct solar penetration; reduce solar heat gain; reduce radiant surface temperatures; control penetration of the solar ray, optimize the interior natural daylighting of a structure and optimize the efficiency of interior lighting systems. The invention additionally comprises a motorized window covering, radiometers, and a central control system that uses algorithms to optimize the interior lighting of a structure. These algorithms include information such as: geodesic coordinates of a building; solar position; solar angle solar radiation; solar penetration angles; solar intensity; the measured brightness and veiling glare across a surface; time, solar altitude, solar azimuth, detected sky conditions, ASHRAE sky models, sunrise and sunset times, surface orientations of windows, incidence angles of the sun striking windows, window covering positions, minimum BTU load and solar heat gain.
Owner:MECHOSHADE SYST LLC

Method for predicting and mitigating power fluctuations at a photovoltaic power plant due to cloud cover

A method for forecasting reduction in sunlight intensity due to cloud cover at a photovoltaic power plant is described. The method comprises determining characteristics of one or more clouds from sensors surrounding the photovoltaic power plant. The cloud characteristics are used to create a 3D map of the clouds. The 3D map in combination with information on the angle of the sun is used to create a 3D projection on the surface of the earth, resulting in a 2D surface irradiance map. The 2D surface irradiance map may be taken in successive projections or used in combination with wind speed data to forecast fluctuation in irradiance at the photovoltaic power plant. The forecasted reductions in power may be used to enact measures at the plant such as reducing the power output of inverters to prevent sudden fluctuations in the power output of the photovoltaic plant feeding the utility.
Owner:TMEIC

Positioning system using light information

An apparatus and method for initiating a search mode of a mobile device based on the light information in the environment of the mobile device is described herein. The light information may include at least one of color temperature or illuminance, which may be used to determine if the environment of the mobile device is indoors or outdoors. A threshold may be predetermined or adjusted based on received position assistance information. The position assistance information may include at least one of time, day, solar angle, motion information, location information, or weather information.
Owner:QUALCOMM INC

Method for improving orbit-transferring safety of inclined orbit satellite

The invention relates to a method for improving the orbit-transferring safety of an inclined orbit satellite, wherein the problem of energy-source shortage of the inclined orbit satellite in the period of orbit-transferring motorization under the condition of high solar angles is solved through the reasonable adjustment of flight events by considering the condition of solar altitude angles in the designing process of a flight program, and meanwhile, flight-control operation can be simplified. The discharging time of a storage battery in the period of orbit-transferring ignition can be shortened by designing the flight program according to the method, so that the load power in the power-supplying period of the storage battery is reduced, therefore the discharging depth of the storage battery is reduced, the energy-source safety of the satellite is ensured, and a launch window is not limited by solar illumination angles.
Owner:BEIJING INST OF SPACECRAFT SYST ENG

Precision compensation method for area APS (active pixel sensor) digital sun sensor

ActiveCN102435204AImprove angle calculation accuracyCompatible calculation methodMeasurement devicesCMOS sensorImaging processing
The invention which discloses a precision compensation method for an area APS digital sun sensor belongs to the spacecraft attitude control measure system field. The precision compensation method comprises the small-angle incidence angle precision compensation and the wide-angle incidence angle precision compensation. The precision compensation method comprises the following steps: 1, carrying out primary rotation correction on the solar faculae center coordinate value which is obtained through the calculation of a sun sensor image processing chip and is input by the sun sensor image processing chip; 2, carrying out secondary correction on the coordinate value of the wide-angle incidence angle, and utilizing the rotarily-corrected coordinate value to do the coordinate mapping of a refraction model; 3, calculating through an uniaxial higher-order polynomial fitting process to obtain the solar angle tangent value, utilizing the rotarily-corrected coordinate value to calculate if the incidence angle is a small angle, and utilizing the secondarily-corrected coordinate value to calculate if the incidence angle is a large angle; and 4, finding the arc tangent to obtain the sun angle value. The precision compensation method which is suitable for the precision compensation of the area APS array digital large-field sun sensor has the advantages of major error factor compensation and high precision.
Owner:TSINGHUA UNIV

Error correction method and device for digital sun sensor

The invention discloses an error correction method for a digital sun sensor. The method comprises the following steps of: 1, determining a proportional correction factor of a theoretical measured value and an actual measured value of a distance from a projection center of a speckle produced by a light introducer on an image sensor to an imaging point during vertical incidence of sunshine; 2, establishing an iterative equation; and 3, performing iterative computation to correct errors, selecting a measured value of a sunshine incident angle as an initial angle of iteration, converging to obtain the value of the angle so as to solve the correction factor in the step 1, and finally correcting the measured value according to the formula of the first step so as to obtain the theoretical measured value. The invention also provides a digital sun sensor based on the method, which can quickly and accurately correct errors and has resolution of 0.02 degree and two axial vision angles of 120 degrees. Thus, power consumption is greatly reduced, data refresh rate is increased, cost is reduced, and high-accuracy solar angle measurement in a large vision angle range is realized.
Owner:北京天银星际科技有限责任公司

Satellite yaw controlling and guiding method

InactiveCN105539884ASatisfy the daily accuracy requirementsConducive to the implementation of thermal controlCosmonautic vehiclesSpacecraft guiding apparatusSolar angleYaw control
The invention provides a guide rule designing method in yaw gesture control over a satellite. The method comprises the following steps that firstly, the track solar angle (an angle beta for short) and a sun vector under a track system are calculated; secondly, when the angle beta is larger than or equal to a given threshold value, a target yaw angle is calculated according to a current track system sun vector, and when the angle beta is smaller than the given threshold value, the target yaw angle is calculated according to a hypothesis sun vector with the angle beta being an assigned angle; thirdly, when the angle beta crosses zero and when it is met the condition that the target yaw angle is a small angle at the same time, a calculation method of the target yaw angle is switched.
Owner:SHANGHAI ENG CENT FOR MICROSATELLITES

Method for obtaining satellite solar angle and time on basis of satellite orbit characteristics

A method for obtaining satellite solar angle and time on the basis of satellite orbit characteristics comprises the following steps: (1) according to the satellite sun-synchronous orbit characteristics, calculating the orbit inclination angle from the height of the satellite orbit; (2) according to the number of satellite orbits, calculating the longitude and Beijing time of sub-satellite point of the position where a satellite descending orbit intersects the equator, and converting the Beijing time into the local time so as to obtain the time of the position; (3) calculating to obtain the local times of any latitude where the satellite sub-satellite point pass; (4) according to the orbit injection error of satellite orbit inclination angle and the daily change rate of satellite orbit inclination angle during the operation process, calculating to obtain the change of satellite local time and actual local times of any latitude; (5) calculating to obtain the actual local time after satellite side-sway; (6) calculating to obtain the solar altitude, solar azimuth, and the Beijing time of an observation site. The provided method can precisely obtain the solar altitude, solar azimuth, and imaging time of a satellite according to a remote sensing satellite nominal orbit and changes thereof without knowing the satellite ephemeris data and specific imaging time.
Owner:CHINA CENT FOR RESOURCES SATELLITE DATA & APPL

Self-power wireless simulation solar angle sensor

The invention provides a self-power wireless simulation solar angle sensor, belonging to the spacecraft attitude measurement sensor technical field. The sensor is characterized in that the sensor comprises a solar angle sensor unit, a power support unit and a wireless communication unit. The solar angle sensor unit comprises four parts of a front end optical system, a solar angle sensor, a conditioning circuit and an external cavity body. The power support unit comprises two parts of a power collecting device and a power management circuit. The wireless communication unit comprises an A / D converting circuit which is connected with the conditioning circuit and used for receiving solar angle information and a wireless communication circuit. The self-power supply and the pure wireless simulation solar sensor are realized in the invention. A two-dimensional position sensitive detector (PSD) is adopted as the solar angle sensor which has the advantages of high precision, simple structure, small size and no externally physically connected electric interface. Therefore, the self-power wireless simulation solar angle sensor is beneficial for the integrated design of an application system.
Owner:TSINGHUA UNIV

Solar panel angle regulation device for curbside small retailer cart

The invention relates to a curbside small retailer cart, in particular to a solar panel angle regulation device for the curbside small retailer cart. The solar panel angle regulation device for the curbside small retailer cart is characterized by being capable of flexibly regulating an angle of a solar panel, higher in solar utilization rate and high in practicability. The solar panel angle regulation device for the curbside small retailer cart comprises a ceiling, a storage battery, a guide wheel, a support rod, first springs, an installation plate, a solar panel, installation blocks, slide rails, slide blocks, second springs and first connection rods, wherein the storage battery, the guide wheel and the support rod are sequentially arranged at the bottom of the ceiling from left to right. The solar panel angle regulation device can flexibly regulate the angle of the solar panel through a steel wire rope and is also simple to operate, and the solar panel is longer in light receiving time and more in light amount by adjusting the angle of the solar angle.
Owner:临沂港控能源有限公司

Solar power collection with near infrared wideband reflector coating

A near infrared (NIR) wideband reflector coating designed to start reflecting solar energy wavelengths from at least 1.2 microns in a typical geosynchronous earth orbit or medium earth orbit satellite and from at least 1.3 microns in a typical low earth orbit satellite. Also, the (NIR) wideband reflector coating reflects solar energy wavelengths below 0.35 microns in all three applications. This invention works on triple junction (TJ) solar cells. The performance of at least 1.2-microns is on solar panels with near-normal incident solar angle, typical of Geosynchronous Earth Orbit (GEO) and Medium Earth Orbit (MEO) satellites. The performance of at least 1.3-microns is on solar panels with wide range of incident solar angles, a design requirement for Low Earth Orbit (LEO) satellites.
Owner:THE BOEING CO

Method for controlling the attitude of an satellites in elliptic orbits using solar radiation pressure

The present invention provides a method for the attitude control of satellites in elliptic orbits or satellites initially placed in circular orbits perturbed to elliptic orbits due to environmental disturbances. The method relies on the application of solar radiation pressure to provide the desired torque for the satellite attitude control. The satellite is equipped with two-oppositely placed light-weight solar panels extending away from the satellite along a predetermined direction (satellite body fixed Y-axis). By rotating one of these solar panels or both of them through desired angles about their axis using the respective driver motors as per the simple open-loop control law, the torque about the satellite axis is developed to achieve the desired attitude performance. The open-loop control law is derived using an analytical approach to neutralize the excitation caused by eccentricity and it is implemented via analog logic based on the information of sun angle and satellite position provided by the sensors. The present invention significantly improves the performance of the satellite by a factor of more than 20 times approximately in general and it only requires the rotation of the solar panels by fraction of a degree for particular system parameters. Thus, the semi-passive nature of the present invention makes it attractive for future space applications.
Owner:KOREA ADVANCED INST OF SCI & TECH

Satellite configuration design method adapting to one-rocket multi-satellite launching

The invention relates to the field of satellite development, in particular to a satellite configuration design method adapting to one-rocket multi-satellite launching. According to the method, for the illumination characteristic that the solar angle of a low-dip-angle orbit changes in a large range, an outer surface corresponding to the lower bottom of a satellite trapezoidal cross section is improved to be an arch formed by three panels in an enclosing mode to serve as an installing surface for fixing a solar cell array, and iterative optimization is conducted on included angles of the three cell panels. A satellite configuration designed through the method can be equivalent to the satellite configuration formed by a prismoid with a trapezoidal cross section and two slant prismoids with trapezoidal cross sections. The satellite configuration design method adapting to one-rocket multi-satellite launching has the main advantages that a solar wing spreading and driving mechanism is not arranged for each satellite, the weights of the satellites are reduced, and the reliability of the satellites is improved; a flight mission of long-time over-the-ground three-axis stable operation of a low-oblique-angle orbit can be met.
Owner:AEROSPACE DONGFANGHONG DEV LTD

Solar angle-adjustable solar streetlamp power generation device

The invention relates to solar power generation devices, in particular to a solar angle-adjustable solar streetlamp power generation device. The solar angle-adjustable solar streetlamp power generation device can automatically clean a solar panel, is high in lighting efficiency and simple in structure. The solar angle-adjustable solar streetlamp power generation device comprises a streetlamp, a swing base, a placing plate, a solar panel, a supporting plate, a collection box, a net plate, a water collection bucket and the like; the swing base is arranged on the top of the streetlamp, and the placing plate is connected to the swing base. Through the water collection bucket, rainwater is subject to flow guide, and is stored through a water tank, through a water pump, water in the water tank is sprayed to the surface of the solar panel, a cleaning mechanism is used for auxiliary cleaning of the solar panel, through a water accumulating tank and a guide pipe, water drops flowing out are subject to flow guide, the solar panel can be automatically cleaned, the lighting efficiency is improved, and the structure is simple and reliable.
Owner:谭令华

Digital sun sensor for stable-spinning micro/nano satellite

A digital sun sensor for stable-spinning micro / nano satellite comprises a detector, an instruction seam, a measuring seam and an electric circuit processing subsystem, wherein the detector is formed with two groups of orthogonal photoelectric coded discs by four photoelectric coded discs and comprises two vertical photoelectric coded discs and two horizontal photoelectric coded discs. The instruction seam is vertical with the measuring seam. The sun light vertical with the measuring seam penetrates the measuring seam and irradiates to the photoelectric coded discs. A voltage signal is output after the sensitization of the photoelectric battery. The included angle between the solar vector direction and the spinning shaft direction of the satellite can be obtained through executing amplifying, comparing, quantifying and matching processing to the signal by the circuit processing subsystem. The invention realizes the digital sun sensor which has the advantages of large viewing field, high precision, small volume and simple structure, and has important practical meaning for realizing high-precision solar zenith measuring by the stable-spinning micro / nano satellite.
Owner:BEIHANG UNIV

Spacecraft energy-complementing system based on sunlight reflection

A spacecraft energy-complementing system based on sunlight reflection comprises an energy-complementing serving spacecraft which projects the sunlight to a battery cell which does not face the sunny side according to the space relation between the sun and a served spacecraft, and extra energy is provided for the served spacecraft. The energy-complementing serving spacecraft comprises a spacecraft body, a sun sensor, a sunlight reflector and a target guiding device. The sun sensor is used for measuring the incoming solar angle, the target guiding device is used for measuring the relative dimensional orientation between the served spacecraft and the energy-complementing serving spacecraft, a star computer on the energy-complementing serving spacecraft is used for calculating the pointing of the sunlight reflector according to the incoming solar angle and the relative dimensional orientation, the sunlight reflector is driven by controlling the attitude maneuver of the energy-complementing spacecraft to arrive at the appointed direction, and the sunlight reflector is used for reflecting the sunlight to the solar cell which does not face the sunny side of the served spacecraft.
Owner:CHINA ACADEMY OF SPACE TECHNOLOGY

Method and system for tracing solar angles of solar lighting boards

The invention relates to a method and system for tracing solar angles of solar lighting boards. The method comprises the following steps of: (1) arranging a plurality of solar lighting boards in an array; (2) installing a solar angle detector on a main board, wherein one lighting board in the array is selected as the main board, and the rest ones are taken as slave boards; (3) controlling the elevation and the azimuth of the main board in a manner that a hydraulic pump drives an ejector rod of a hydraulic oil cylinder; (4) converting the elevation and the azimuth of the main board to two voltage signals with different frequencies by an angle sensor of the main board, and transmitting the voltage signals to control circuits of the slave boards in a time division manner; and (5) performing rectification by the control circuit of each slave board according to the voltage signals with the different frequencies received in a time division manner, and adjusting the gestures of the slave boards in a manner that the hydraulic pump drives the ejector rod of the hydraulic oil cylinder so as to ensure that the slave boards and the main board are same in elevation and azimuth. The system is simple in structure and low in cost and energy consumption, has a good tracing effect, is beneficial to the great improvement on a utilization rate of solar energy, and is energy-saving and environment-friendly.
Owner:福建恒昌电子科技有限公司

Solar street lamp structure with adjustable angle

The invention relates to a solar street lamp structure with an adjustable angle, which comprises a street lamp holder, a light-emitting unit, a solar panel, a power accumulating part and a braking part, wherein a bracket of the street lamp holder is movably combined with a bearing part through a coupling unit, and the power accumulating part is arranged in the street lamp holder; and a braking unit of the braking part is arranged between the bracket and the bearing part, thus the braking part can adjust the angle between the bearing part and the bracket through the braking unit so that the light-emitting unit and the solar panel which are arranged at the bearing part can be adjusted synchronously. Thus, the solar panel can be adjusted with the solar angle to increase the power generation efficiency, and the light-emitting unit can also be adjusted to change the illumination direction of the solar street lamp structure, thereby achieving the effect of extending the application range of the solar street lamp structure.
Owner:POWER LIGHT TECH

Efficient solar energy automatic tracking method and device

ActiveCN103926937AImprove the efficiency of absorbing light energyImprove tracking efficiencyControl using feedbackSolar angleEngineering
The invention relates to an efficient solar energy automatic tracking method and device. The method includes the steps that first, the outside weather condition is judged, if it is sunny, a photoelectric detection tracking mode is adopted to achieve solar energy automatic tracking, and if it is cloudy or illumination is not sufficient, a sun angle tracking mode is adopted, and in other words, the solar altitude and the azimuth angle are calculated according to real-time time, and solar energy automatic tracking is achieved according to the calculated solar altitude and the calculated azimuth angle. According to the method and device, a photoelectric detection tracking method is combined with a sun angle tracking method, a solar cell panel can change along with changes of the solar altitude and the azimuth angle, the solar cell panel can be kept perpendicular to solar rays all the time, and therefore the efficiency of solar cells is improved. Not only can the sensitivity of the solar energy tracking device be improved, but also interference of weather and other light sources can not happen to the device easily, and the device is high in stability and small in error.
Owner:STATE GRID CORP OF CHINA +2

Folding solar automatic tracking device

The invention discloses a folding solar automatic tracking device. The device comprises a control system, a containing box, a multilevel laminated solar wing, a driving device, an adjusting device anda folding support. The control system comprises a single-chip microcomputer control module, a photoelectric detection tracking module and a solar angle tracking module. The photoelectric detection tracking module realizes solar automatic tracking through detecting illumination information. The solar angle tracking module realizes the solar automatic tracking through calculating a real-time solarazimuth and an elevation angle. The single-chip microcomputer control module controls orientation of the multilevel laminated solar wing through the adjusting device. The multilevel laminated solar wing is folded, after being folded, the folding support, the driving device and the adjusting device are arranged in a box body. In the invention, tracking efficiency is increased, a light absorption surface of the solar wing is guaranteed to be vertical to solar incident rays under different weather states and different illumination orientations, repeated unfolding and folding motion of the solar wing is realized and an outdoor power generation supply problem is solved.
Owner:SHANDONG UNIV OF SCI & TECH

Control circuit of solar power generation tracking system

The invention discloses a control circuit of a solar power generation tracking system. The control circuit of the solar power generation tracking system mainly consists of a tracking module, a single chip microcomputer controller, a driving unit and an energy conversion unit. The tracking module integrates photoelectric tracking and sun angle tracking, wherein the sun angle tracking is adopted at the first stage, and a photoelectric sensor is adopted at the second stage to correct tracking. The driving unit drives a stepping motor to run and respectively controls pole-around shaft rotation and pitch angle adjustment to achieve automatic sun tracking. The energy conversion unit utilizes a Stirling heat engine to convert solar energy heat into mechanical energy and utilizes a Stirling motor to convert the converted mechanical energy into electric energy. Wind speed and direction, illumination intensity and solar cell parameters are detected in real time while tracking. The receiving rate of a photovoltaic cell can be greatly improved, solar energy resources can be effectively and fully utilized, and the solar energy application field is widened.
Owner:XIAN ZHONGKEMAITE ELECTRONICS TECH EQUIP

Magnetic control sun capturing method in consideration of solar angle change rate and variable control factor weight

The invention discloses a magnetic control sun capturing method in consideration of a solar angle change rate and a variable control factor weight. The method comprises the steps of calculating a solar angle, a solar angular velocity and modulus of a magnetic vector change rate; performing sun vector calculation validity determining; when sun vector calculation is effective, performing moment application direction calculation based on a flywheel rotation starting offset finishing condition; performing magnetic moment application direction calculation, and calculating an included angle betweenthe magnetic moment and the moment direction; determining whether the included angle between the magnetic moment and the moment direction is in a range between an upper limit and a lower limit; when the included angle between the magnetic moment and the moment direction is in the range between the upper limit and the lower limit, calculating a magnetic control output according to a rate and solarangle control and solar angle speed compensation algorithm; and performing amplitude limitation on a magnetic control output magnetic moment.
Owner:SHANGHAI ENG CENT FOR MICROSATELLITES

APS digital sun sensor sun angle calculating method and system

The invention discloses an APS digital sun sensor sun angle calculating method. The sun angle calculating method comprises the steps that the sun facula position of a digital sun sensor is read; an initial sun incidence angle is calculated according to the sun facula position; iterative computation is performed by combining the initial sun incidence angle with the calibration parameters of the digital sun sensor to obtain a sun incidence angle; a corrected two-dimensional sun angle is calculated. The APS digital sun sensor sun angle calculating method greatly improves the sun angle calculation accuracy through sun angle correction and iterative computation of the sun sensor and facilitates improvement of satellite attitude precision.
Owner:SHANGHAI AEROSPACE CONTROL TECH INST

A satellite configuration design method suitable for multi-satellite launch with one rocket

The invention relates to the field of satellite development, in particular to a satellite configuration design method adapting to one-rocket multi-satellite launching. According to the method, for the illumination characteristic that the solar angle of a low-dip-angle orbit changes in a large range, an outer surface corresponding to the lower bottom of a satellite trapezoidal cross section is improved to be an arch formed by three panels in an enclosing mode to serve as an installing surface for fixing a solar cell array, and iterative optimization is conducted on included angles of the three cell panels. A satellite configuration designed through the method can be equivalent to the satellite configuration formed by a prismoid with a trapezoidal cross section and two slant prismoids with trapezoidal cross sections. The satellite configuration design method adapting to one-rocket multi-satellite launching has the main advantages that a solar wing spreading and driving mechanism is not arranged for each satellite, the weights of the satellites are reduced, and the reliability of the satellites is improved; a flight mission of long-time over-the-ground three-axis stable operation of a low-oblique-angle orbit can be met.
Owner:AEROSPACE DONGFANGHONG DEV LTD

Solar classroom

The invention discloses a solar classroom applicable to solar energy supply. Taking a four-storey teaching building as an example, the solar classroom is characterized in that solar cell panels (1) are arranged on a southern wall, a western wall and roof balconies of the solar teaching building and can be controlled by an industrial controller (3) to be adjusted according to change of the solar angle, so that sunlight can be absorbed to the greatest extent; Fresnel lenses (2) are arranged at edges of a roof, reflectors (2) are arranged on the outer side of each storey of the building, and concave lenses (16) are arranged in each classroom; light rays are gathered via the Fresnel lenses (2), and are guided to the concave lenses (16) in the classrooms via light tanks and the reflectors (2), and each integral classroom is brightened; and the brightness of the inside of each classroom can be controlled by adjusting angles of the Fresnel lenses (2) via the industrial controller (3).
Owner:NANJING DAWU EDUCATION TECH

Method and device for determining azimuth angle of photovoltaic string and electronic equipment

PendingCN114461976AReduce workloadImprove efficiency in determining PV string azimuthData processing applicationsSystems intergating technologiesSolar angleEngineering
The invention provides a photovoltaic string azimuth angle determination method and device and electronic equipment, and the method comprises the steps: obtaining a power generation performance data sequence of a photovoltaic string and sun angles at different moments, and the power generation performance data sequence comprises power generation performance data of the photovoltaic string at different moments; determining a maximum data moment corresponding to maximum power generation performance data in the power generation performance data sequence, and establishing an objective function according to the sun angle and the power generation performance data at each moment; and determining the string azimuth angle of the photovoltaic string according to the maximum data moment and the objective function. According to the technical scheme, the workload and labor cost for determining the azimuth angle of the photovoltaic string are reduced.
Owner:HEFEI SUNGROW RENEWABLE ENERGY SCI & TECH CO LTD

Wireless self-powered digital sun sensor

The invention provides a wireless self-powered digital sun sensor comprising a power module, an MEMS (micro electro mechanical system) light leading-in device, a CMOS (complementary metal oxide semiconductor) image detector and an electronic system, wherein the power module is used for supplying power to the wireless self-powered digital sun sensor; the MEMS light leading-in device comprises at least one group of asymmetrical hole patterns; the CMOS image detector is located below the MEMS light leading-in device and used for detecting light led by the MEMS light leading-in device and outputting row light intensity information of a sensing unit of the detector; the electronic system is used for managing energy supplied by the power module, calculating solar angles of two axes according to the row light intensity information and outputting the solar angles of two axes to an upper computer. The sun sensor is high in minimization and autonomous modularization degree, flexible and convenient to use, self-powered, capable of realizing wireless communication and capable of improving the measurement calculation accuracy of the solar angles of the two axes.
Owner:TSINGHUA UNIV

Tracking method and device for solar tracker

The invention provides a tracking method and device for a solar tracker. The method includes: controlling a solar panel of the solar tracker to move to a first place according to the current time parameters and the current position of the solar tracker; determining the second position of the solar panel according to the parameters obtained by a solar angle sensor of the solar tracker; judging whether the corresponding angle difference of the second position and the first position is in the preset angle range; rectifying the corresponding angle of the first position subject to the corresponding angle of the second position when the corresponding angle difference of the second position and the first position is in the preset angle range according to judgment. By means of the tracking method and the tracking device, the problem that the system is unstable caused by the fact that the hybrid control solar tracker in the prior art is greatly influenced by the environment, and the effect of improving the stability of the solar tracker is improved.
Owner:中天同圆太阳能高科技有限公司
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