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37 results about "Analytic relation" patented technology

Method for regulating voltage of key node of grid polymerization based on measurement of phasor measurement unit

The invention discloses a method for regulating voltage of key node of grid polymerization based on measurement of a phasor measurement unit in a wide-area environment. The method is characterized by comprising the following steps: analyzing a relation between voltage vectors and current vectors of nodes, analyzing a relation between the voltage vectors of the nodes and power, regulating voltage of the key node of a polymerization grid in the wide-area environment, and solving a key node voltage regulating model by a nonlinear least square method. According to the method, the analytic relation between the voltage vectors of the nodes and the power is obtained by virtue of the relation between the voltage vectors and the current vectors of the grid nodes; the definition of grid polymerization and a regulation relation between the voltage vectors of the nodes and the power are obtained on the basis of the analytic relation in the wide-area measurement environment; a regulation equation for grid polymerization to the key node is further obtained without taking an out-of-limit power transmission circuit trend into account. The method is scientific and reasonable as well as simple and feasible, and is accurate in regulation, high in applicability and suitable for simplified analysis, on-line monitoring and real-time control of the grid.
Owner:STATE GRID CORP OF CHINA +2

Zoning-based combined approximate model building method

The invention relates to a zoning-based combined approximate model building method which has high adaptability to unknown linear and nonlinear problems. The zoning-based combined approximate model building method is characterized in that a combined approximate model is built under the condition that the input values and the output values of a certain number groups are given to approximate the input and output analytic relation of a system, and the output of the system is forecasted under the condition that the input of the system is given. The zoning-based combined approximate model building method is mainly applied to approximation of the functional relation between optimization objectives and variables during optimal design. As for the problem that the strong linear or nonlinear features of local areas cannot be well captured because traditional approximate models adopt modeling on the whole test area, the concept of modeling by dividing the whole test area is adopted. On one hand, the precision forecasting advantage of the combined approximate model to a single approximate model is utilized, and on the other hand, the purpose of improving the forecasting precision to the local area is achieved, so that the overall forecasting precision of the model is improved. Therefore, the computing time and resources, consumed by iterative optimal solution solving, can be greatly shortened and reduced in the optimization process.
Owner:BEIHANG UNIV

Spacecraft high-precision angular motion measuring method based on rotor-type gyroscope biorthogonal configuration

The invention relates to a spacecraft high-precision angular motion measuring method based on rotor-type gyroscope biorthogonal configuration, and belongs to the technical filed of inertial navigation. An analytic relation including the posture angular rate and angular acceleration information of a spacecraft is obtained by utilizing resultant external moment radially borne by a gyroscope rotor, under the situation that an inertial coupling item and a cross coupling item caused by spacecraft angular motion are not neglected, the inertial coupling item and the cross coupling item are eliminatedthrough information fusion operation of a plurality of gyroscopes in the biorthogonal configuration, and thus the analytic relation including the angular rate and the angular acceleration of the spacecraft is obtained in a combined mode. Due to the fact that the inertial coupling item and the cross coupling item are reserved, the measuring precision of the spacecraft high-precision angular motionmeasuring method only depends on a gyroscope error and a configuration mounting error and is not lowered with increasing of the dynamic range of the spacecraft. According to the spacecraft high-precision angular motion measuring method, the prominent contradiction between the measuring precision and the dynamic range in a traditional posture angular rate and angular acceleration measuring methodis effectively overcome. The spacecraft high-precision angular motion measuring method can be applied to high-precision and high-bandwidth measuring of the angular rate and the angular acceleration ofthe spacecraft.
Owner:任元 +1

Gaussian filtered minimum shift keying (GSMK) digital demodulation error metering method and system

The invention relates to a Gaussian filtered minimum shift keying (GSMK) digital demodulation error metering method and a system. The metering method comprises the steps of: 1) taking a phase modulation (PM) signal as a standard GSMK signal; 2) setting 0.5Rs difference value delta f by setting the modulation frequency and standard of the PM signal, and setting the capture length N of a vector signal analyzer at the same time, wherein the N and the delta f satisfy a certain constraint relation; 3) establishing an analytic relation between the frequency parameter delta f and a modulation error parameter; and 4) comparing the calculable digital modulation error parameter with a value measured by the vector signal analyzer to realize the metering and calibration of a GMSK demodulation error parameter. The metering system provided by the invention comprises an analog signal generator, a power divider, a tunable receiver and a measured vector signal analyzer. The method and the system provided by the invention can be used for metering and calibrating the digital demodulation errors of vector signal analyzers and mobile communication comprehensive testers with a GMSK analysis and demodulation function, and can be widely used.
Owner:TELECOMM METROLOGY CENT OF MINIST OF IND & INFORMATION TECH +1

Method of predicting service life of power cell based on big data

The present invention discloses a method of predicting service life of a power cell based on big data. Parameter big data of the same type of the power cell are measured randomly under a different depth of discharge, a different temperature and a different rate of discharge. Big data analysis is performed on the parameter big data to obtain an analytic relation of the big data. Current big data are measured by a voltage-current sensor, simultaneously an improved Amp-hour integral method is adopted to obtain a State of Charge (SOC) and the depth of discharge is obtained from the relation withthe sum of the depth of discharge and the SOC being 1. Under a different depth of discharge, the throughput of one charging and discharging of the cell is equivalently deemed as an equivalent throughput. According to the equivalent throughput and a rated throughput, the residual service life of the cell can be calculated. The prediction method of the present invention, from characteristics of thepower cell, corrects the throughput of an effective charging and discharging with regard to the depth of discharge, an ambient temperature and the size of discharging current. Meanwhile, according tothe characteristics of the power cell, the method optimizes test of an initial SOC, thereby making a prediction result more accurate.
Owner:复变时空(武汉)数据科技有限公司

Method for generating safe launching window of weak-gravitation small celestial body surface lander

The invention discloses a method for generating a safe launching window of a weak-gravitation small celestial body surface lander, and belongs to the technical field of deep space exploration. The implementation method comprises the steps of: firstly, defining a landing point tangent normal coordinate system of a small celestial body, and deriving the analytical relation among the launching state,the landing state and the landing time of a lander near the small celestial body; secondly, establishing a launching constraint meeting the safety rising requirement of a main detector and a landingconstraint meeting the safety landing requirement of the lander on a tangent system, and defining a launching window; then, deducing a two-dimensional projection boundary analytic expression of a window of the landing speed constraint on a two-dimensional plane according to the landing dynamics analytic relation and the launch landing constraint; and finally, designing evaluation indexes representing landing safety to obtain a safe launching window with index distribution. The generated safe launching window can provide a basis for rapid selection of the launching state of the lander, and thelanding safety and the landing success rate are improved.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY
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