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38results about How to "The derivation process is simple" patented technology

Multi-step decision-making method for planning trajectory around multiple no-fly zones

The invention relates to a multi-step decision-making method for planning a trajectory around multiple no-fly zones. The method comprises the following steps of 1 impact point prediction calculation,2 boundary constraint handling scheme, 3 orientation adjustment scheme, 4 proportional navigation and 5 implementation of the method for planning the trajectory around multiple no-fly zones on the basis of a multi-step decision-making theory. Compared with an off-line planning method, the trajectory planning method has the advantages that the real-time performance is high, the on-line planning speed is high, and new avoiding instructions can be generated in real time according to the task and battlefield environment requirements; and compared with a traditional on-line planning method, the trajectory planning method has the advantages that the derivation process is simple, the condition of a large amount of randomly-distributed no-fly zones can be processed, and the trajectory planning method has the higher adaptability. According to the trajectory planning method, boundary constraints of the no-fly zones can be strictly guaranteed, a flying trajectory is smooth, the required overloadis small, and the trajectory planning method has the higher guidance precision.
Owner:BEIHANG UNIV

Pesticide freshwater aquatic organism water quality benchmark value derivation method and water quality safety assessment method

The invention belongs to the technical field of water quality safety assessment, in particular to a pesticide freshwater aquatic organism water quality benchmark value derivation method and a water quality safety assessment method. The pesticide freshwater aquatic organism water quality benchmark value derivation method disclosed by the invention includes data collection, data screening evaluation, species screening, water quality benchmark derivation and benchmark value checking, when evaluating whether a certain water quality is safe or not, the water quality benchmark value for protecting aquatic organisms is obtained according to the aquatic organism water quality benchmark derivation procedure, and then the concentration value of such pollutants in the surface water source to be detected is detected. If the concentration value is lower than the water quality benchmark value, the water quality is safe, otherwise, the water quality is unsafe. The water quality benchmark derivation method provided by the invention has strong pertinence and wide applicability, and provides a theoretical basis for the environmental protection department to formulate the water quality standard of the pesticide surface water for protecting aquatic organisms in China.
Owner:CHINESE RES ACAD OF ENVIRONMENTAL SCI

Transformer distribution parameter based LCC resonant type electrostatic precipitator high-frequency high-voltage power supply

The invention discloses a transformer distribution parameter based LCC resonant type electrostatic precipitator high-frequency high-voltage power supply. The power supply comprises a three-phase rectifier bridge, an input filter capacitor, a full-bridge inversion circuit, an LCC serial-parallel resonant circuit, a high-frequency boosting transformer and a high-voltage silicon stack rectifier bridge which are connected in sequence; the three-phase rectifier bridge is electrically connected with three-phase alternating current; and the high-voltage silicon stack rectifier bridge is connected with a load. According to the power supply, the influence on a circuit from the high-frequency transformer distribution parameters is taken into full consideration; the LCC serial-parallel resonant circuit is designed by a fundamental wave analyzing method; the switch-on and switch-off of the zero voltage and zero current of a switch tube can be realized, so that the power switching tube is protected, the EMI noise is lowered, the switch loss is reduced, the switch frequency is improved, and the size of the power supply is reduced; meanwhile, the system is subjected to intermittent power supply control, so that sparks and back corona are effectively prevented; and in addition, the power supply is low in switch loss, relatively smaller in size, low in electromagnetic interference, and high in transmission efficiency.
Owner:ZHENJIANG TIANLI TRANSFORMER

Elastic torque control device

The invention discloses an elastic torque control device. The device comprises an angle sensor, a connecting plate, a shell and an input motor. A servo coder is arranged on the input motor, and the connecting plate is fixedly connected with the shell. The angle sensor is rotationally connected with the connecting plate; one end of a middle connecting piece is connected with the angle sensor, and the other end of the middle connecting piece is connected to a rotating shaft of the input motor. An inner ring of a bearing is coaxially and rotatably connected with the middle connecting piece, and an outer ring is connected with the shell. A plurality of extension springs are further arranged at the side, away from the angle sensor, of the shell. One end of each tension spring is fixedly connected with the shell, and the other end of each tension spring is fixedly connected with the middle connecting piece. The common extension springs are adopted as the elastomers, and the mathematical model derivation is simple. The permissible torque is controlled and output through the servo motor, and the servo motor control method is mature, and the control precision is high. The device is simple in structure and low in cost, and the extension springs can be replaced at any time to change the rigidity of the elastomers. The device is high in universality, and the output actual torque can be accurately controlled through simple calculation.
Owner:INST OF INTELLIGENT MFG GUANGDONG ACAD OF SCI

Method for quickly analyzing landing load of support arm type undercarriage

The invention belongs to the technical field of aircraft structural strength design load analysis, and particularly provides a method for quickly analyzing landing load of a support arm type undercarriage. According to the method, a large-side-angle support arm type undercarriage structure is simplified into a mass-spring system on the basis of the energy conservation principle, in the system, theweight of an airplane is simplified and concentrated to be M, the large-side-angle support arm type structure is simplified into a spring model, tires are simplified into a spring model, and connection of support arms and the tires is simplified into series connection of two springs; an energy equation for simplifying the large-side-angle support arm type structure into the spring model is solved, and an energy equation for simplifying the tires into the spring model is solved; and then, the obtained energy equation is substituted into an energy conservation equation, the maximum vertical load of the landing load of the undercarriage is solved, and the loads in the lateral direction and the heading direction on the undercarriage during landing is calculated. According to the method provided by the invention, a complex calculation model does not need to be established, the derivation process is simple, the obtained landing load is effective and reliable, and the requirements of engineering design can be met.
Owner:CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA

A multi-step decision-making trajectory planning method around multiple no-fly zones

The invention relates to a multi-step decision-making method for planning a trajectory around multiple no-fly zones. The method comprises the following steps of 1 impact point prediction calculation,2 boundary constraint handling scheme, 3 orientation adjustment scheme, 4 proportional navigation and 5 implementation of the method for planning the trajectory around multiple no-fly zones on the basis of a multi-step decision-making theory. Compared with an off-line planning method, the trajectory planning method has the advantages that the real-time performance is high, the on-line planning speed is high, and new avoiding instructions can be generated in real time according to the task and battlefield environment requirements; and compared with a traditional on-line planning method, the trajectory planning method has the advantages that the derivation process is simple, the condition of a large amount of randomly-distributed no-fly zones can be processed, and the trajectory planning method has the higher adaptability. According to the trajectory planning method, boundary constraints of the no-fly zones can be strictly guaranteed, a flying trajectory is smooth, the required overloadis small, and the trajectory planning method has the higher guidance precision.
Owner:BEIHANG UNIV

An elastic moment control device

The invention discloses an elastic torque control device. The device comprises an angle sensor, a connecting plate, a shell and an input motor. A servo coder is arranged on the input motor, and the connecting plate is fixedly connected with the shell. The angle sensor is rotationally connected with the connecting plate; one end of a middle connecting piece is connected with the angle sensor, and the other end of the middle connecting piece is connected to a rotating shaft of the input motor. An inner ring of a bearing is coaxially and rotatably connected with the middle connecting piece, and an outer ring is connected with the shell. A plurality of extension springs are further arranged at the side, away from the angle sensor, of the shell. One end of each tension spring is fixedly connected with the shell, and the other end of each tension spring is fixedly connected with the middle connecting piece. The common extension springs are adopted as the elastomers, and the mathematical model derivation is simple. The permissible torque is controlled and output through the servo motor, and the servo motor control method is mature, and the control precision is high. The device is simple in structure and low in cost, and the extension springs can be replaced at any time to change the rigidity of the elastomers. The device is high in universality, and the output actual torque can be accurately controlled through simple calculation.
Owner:INST OF INTELLIGENT MFG GUANGDONG ACAD OF SCI

Decoupling Method for Independent Inverse System of Bearingless Asynchronous Motor

The decoupling method of the independent inverse system of the bearingless asynchronous motor, the original model of the independent torque system and the original model of the independent magnetic levitation system constructed according to the working principle of the bearingless asynchronous motor, respectively establish the no-load torque variable T L The inverse model of the independent torque system and the α and β axis components of the air gap flux linkage of the independent torque system observed by the independent observer of the air gap flux linkage ψ 1α and ψ 1β The inverse model of the independent maglev system, the cross-coupling item in the dynamic change process of the torque winding stator current has been decoupled by the inverse system method, so the current closed loop in the independent torque original system can be omitted, and the inverse system model does not contain difficult The predicted load torque variable can save the torque online identification link in the system implementation, which can effectively simplify the complexity of the overall control system structure of the bearingless asynchronous motor; using the independent inverse system decoupling method in this paper, the independent torque system inverse The model and the inverse model of the independent maglev system and their derivation process are relatively simple, which is convenient for engineering and technical realization.
Owner:HENAN UNIV OF SCI & TECH

Multi-mode failure judgment method suitable for transverse isotropic carbon fibers

The invention belongs to the field of fracture mechanics, and discloses a multi-mode failure judgment method suitable for transverse isotropic carbon fibers, which comprises the following steps: (1) judging the failure form of the transverse isotropic fibers; (2) constructing a fiber shearing and bending failure stress criterion basic model; (3) judging the sign of the normal stress of the failure surface; (4) solving an undetermined coefficient in the basic form by considering a normal stress symbol of a failure surface under fiber shearing and bending failure states respectively; and (5) establishing a finite element model to verify the accuracy of the model. According to the method disclosed by the invention, the axial/transverse performance difference of the fiber and the influence of the normal stress sign of the failure surface on the shearing and bending failure stress state are considered for the first time, so that the failure of the carbon fiber in various loading processes can be accurately judged. The derivation process is simple, program codes are conveniently generated, and the application of the method is beneficial for further improving the prediction precision of the design performance of the composite material component.
Owner:DALIAN UNIV OF TECH

A Linear/Nonlinear Double-layer Insulation Dielectric Interface Polarization Characteristic Analysis Method

The invention discloses a linear / nonlinear double-layer insulation dielectric interface polarization characteristic analysis method, and belongs to the technical field of insulation dielectric. For solving the problems that in the prior art, the theoretical derivation process is complicated and is difficult to obtain an analytical solution, the method comprises a linear insulation dielectric layer and a nonlinear insulation dielectric layer, wherein the linear insulation dielectric layer and the nonlinear insulation dielectric layer are connected in series, the linear insulation dielectric layer is connected with a first electrode lead, the nonlinear insulation dielectric layer is connected with a second electrode lead, and a direct current high voltage U0 is formed between the first electrode lead and the second electrode lead; and the linear / nonlinear double-layer insulation dielectric is represented by a first volt-ampere special effect curve and a second volt-ampere characteristic curve correspondingly, a linear / nonlinear double-layer insulation dielectric is described by an equivalent circuit model, and the voltage value of the linear insulation dielectric layer, a voltagevalue of the nonlinear insulation dielectric layer, a total polarization current value and a time constant value of the linear / nonlinear double-layer insulation dielectric are obtained, and the technical problem that the interface polarization characteristic derivation process of the double-layer insulation dielectric is complicated is solved.
Owner:HARBIN UNIV OF SCI & TECH
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