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309 results about "Dynamic method" patented technology

The dynamic method is a procedure for the determination of the masses of asteroids. The procedure gets its name from its use of the Newtonian laws of the dynamics, or motion, of asteroids as they move around the Solar System. The procedure works by taking multiple position measurements to determine the gravitational deflection caused when two or more asteroids move past each other. The method relies on the fact that the large number of known asteroids means they will occasionally move past one another at very close distances. If at least one of the two interacting bodies is large enough, its gravitational influence on the other can reveal its mass. The accuracy of the determined mass is limited by the precision and timing of the appropriate astrometric observations being made to determine the gravitational deflection caused by a given interaction.

Energy-based method for automatically locating earthquake focus of microearthquake

An energy-based method for automatically locating the earthquake focus of a microearthquake belongs to the field of microearthquake detection, and relates to an earthquake focus locating method used in a microearthquake monitoring system, in particular to an automatic microearthquake locating method and a method for improving the locating accuracy. The invention adopts an earthquake wave dynamic method which is an earthquake locating algorithm based on earthquake wave energy attenuation equation, complicated calculation of energy of the earthquake waves is not required, parameters such as themaximum shake amplitude or quadratic sum of the shake amplitude and the like are adopted to represent energy, and the arrival time of the earthquake waves does not need to be picked up at all, so that problems caused during automatic locating of the earthquake focus of the microearthquake are solved; and as energy difference is taken as the optimized variable, while energy attenuation is in direct correlation with range, the defect that the travel-time difference serving as the optimized variable is only related to the travel-time difference (range difference) but not in direct correlation with the size of the range per se, the external-field locating accuracy, particularly the accuracy in the vertical direction, is improved, and the stability of the locating result is also improved.
Owner:UNIV OF SCI & TECH BEIJING

Anti-noise-interference redundant manipulator path planning method

The invention discloses an anti-noise-interference redundant manipulator path planning method and a system. The method comprises the steps of (1) building a time-varying quadratic planning model according to an actual redundant manipulator parameter index, and introducing a performance index of a redundant manipulator; (2) using a lagrange multiplier method for carrying out optimal value optimization on the time-varying quadratic planning model; (3) designing a standard matrix equality according to an optimization formula; (4) designing a deviation function equation of the system according toan actual physical model system and the standard matrix equality; and (5) designing the anti-noise-interference redundant manipulator path planning method according to the deviation function equationand a power type varying parameter recursion neurodynamics method, wherein a network state solution solved by the method is an optimal solution. According to the anti-noise-interference redundant manipulator path planning method and the system provided by the invention, with the interference of an outside noise environment, an actual motion path of a redundant manipulator can further coincide withan expected path, so that the calculating speed is greatly improved, and the method has the characteristics of high precision, fast convergence, high instantaneity, good robustness and the like.
Owner:SOUTH CHINA UNIV OF TECH

Navigation constellation inter-satellite link transceiver device time delay calibration method

InactiveCN104267408AImplement latency calibrationSatisfy on-orbit real-time measurementSatellite radio beaconingDynamic methodTransceiver
The invention provides a navigation constellation inter-satellite link transceiver device time delay calibration method. The method comprises the steps of adding a bidirectional calibration channel, a medium-frequency switch matrix and a radio-frequency switch matrix on a transceiver device, conducting time-sharing control on the radio-frequency switch matrix and the medium-frequency switch matrix, sequentially enabling every two of a transmitting channel, a receiving channel and the bidirectional calibration channel to be communicated, performing closed loop time delay testing to obtain three time delay values, and finally calculating an absolute time delay Tt of the transmitting channel and an absolute time delay Tr of the receiving channel according to the three time delay values, wherein the time delay amount serves as a transceiver device time delay zero value to be substituted into inter-satellite link time delay measurement data for time delay calibration, and transceiver device time delay calibration is achieved. By means of the navigation constellation inter-satellite link transceiver device time delay calibration method, on-orbit real-time measurement of a transceiver can be achieved, and transceiver device delay calibration can be completed in a single satellite, namely the defect of static testing is avoided. In addition, compared with other dynamic methods, multi-satellite or multi-antenna participated time delay measurement work is not needed.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Method for calculating dynamic characteristics of contactor based on piecewise linear kinetic equation

ActiveCN107862127AResponse Electromagnetic Dynamic CharacteristicsVisualization of dynamic characteristic solution processGeometric CADDesign optimisation/simulationMagnetic tension forceDynamic method
Provided is a method for calculating dynamic characteristics of a contactor based on a piecewise linear kinetic equation, and belongs to the technical field of basic research design of general characteristics of contactors. The method comprises the steps that according to structural features of the contactor, segmentation is conducted on a contactor action process, plane collision and a continuouscollision force model with energy loss considered are used for being equivalent to a collision process, by means of the multi-body system kinematics based on a restrain method and a dynamic method, studying of the collision bounce situation of a contactor mechanical system under the action of external force is completed, and finally, dynamic characteristic calculation of the contactor with collision bounce considered is completed in combination of a coupling calculation method. The method has the advantages that the time-dependent situation of electromagnetic parameters such as the coil current and electromagnetic force in a working process of the contactor can be obtained, the electromagnetic dynamic characteristics of the contactor can be reflected more accurately, and errors are controlled within 5%; the bounce situation of an armature and a moving contact of the contactor can be reflected more really, and errors are controlled within 5%.
Owner:HARBIN INST OF TECH
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