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33 results about "Nonlinear differential equations" patented technology

A linear differential equation is a differential equation (an equation containing a function and its derivatives) where the function and its derivatives: Hence, a nonlinear differential equation is any one that violates any of those two conditions.

Power system transient stability simulating method based on implicit numerical integration

InactiveCN102609575ASmall amount of calculationReduced number of integration step iterationsSpecial data processing applicationsInformation technology support systemTruncation error (numerical integration)Transient state
The invention discloses a power system transient stability simulating method based on implicit numerical integration. Compared with an existing power system transient stability numerical simulation implicit trapezoidal integration method, the power system transient stability simulating method employs a power-angle integration formula with a smaller local truncation error, namely, enables a non-linear differential equation set for describing a power system transient process to be expressed as a linear portion and a non-linear portion. An accurate analysis expression of a state transition matrix is obtained by reasonably selecting a system matrix of the linear portion as a singular matrix, and a group of implicit integration formulas is obtained by leading linear integrable functions to be approximate to the non-linear portion of the differential equation set. The local truncation error of the power-angle implicit integration formulas of the generator refers to O (h5) which is larger than a local truncation error O (h3) of implicit trapezoidal integration, the calculated quantity of integration each time is equivalent to that of the implicit trapezoidal integration. By means of the high-precision implicit integration formulas, iteration times of each integration step under the same iteration precision condition are decreased, so that the simulated calculated quantity is remarkably decreased.
Owner:ZHEJIANG UNIV

Tilt-rotor helicopter control decoupling design method

ActiveCN112182753ASolve the phenomenon of longitudinal control surface redundancyAvoid couplingGeometric CADSustainable transportationLevel flightClassical mechanics
The invention discloses a tilt-rotor helicopter control decoupling design method which comprises the following steps: making an initial longitudinal control strategy of a tilt-rotor helicopter, establishing an aerodynamic force and moment model and a gravity model of a tilt-rotor helicopter component, and obtaining a nonlinear differential equation set based on a six-degree-of-freedom motion equation; according to the nonlinear differential equation set, selecting a rotor wing deflection angle under an interval value, solving the flight trim control quantity of the maximum speed of the tilt rotor wing helicopter and the required engine power, establishing a maximum level flight speed trim result table under different rotor wing deflection angles, and determining a new longitudinal controlstrategy; determining a new level flight speed balancing result table based on the new longitudinal control strategy; selecting a rotor total propeller pitch corresponding to the same steering columnlongitudinal control quantity under different rotor deflection angles in the table, and determining a decoupling coefficient between the rotor deflection angles and the rotor total propeller pitch based on the rotor total propeller pitch; calculating the change of the total pitch along with the inclination angle of the rotor according to the decoupling coefficient so as to solve the total pitch ofthe rotor.
Owner:CHINA HELICOPTER RES & DEV INST

Dish type solar energy concentrator and design method thereof

The invention provides a dish type solar energy concentrator. The bottom of a dish surface is provided with a circular opening, the dish surface is a rotation curved surface, and the bus of the rotation curved surface is a curve based on a specific first-order nonlinear differential equation. Disclosed is also a design method of the dish type solar energy concentrator. According to a light uniform reflection principle and related optical geometry knowledge, the specific first-order nonlinear differential equation bus equation of the rotation curved surface of the dish surface is derived through calculating. According to the dish type solar energy concentrator and the design method thereof, the dish type solar energy concentrator is provided with the dish bottom opening, and the rotation curved surface bus of the dish surface is a specific first-order nonlinear differential equation curve, so that the dish type solar energy concentrator can form quite uniform hot-fluid distribution on a receiver, and the energy conversion efficiency and other integration performance of the concentrator are substantially improved. Therefore, the dish type solar energy concentrator and the design method thereof are especially suitable for an optically focused photovoltaic solar device of a large-dimension receiver.
Owner:HUAZHONG UNIV OF SCI & TECH

Radio energy transmission system tuning feedback control method considering dynamic performance

The invention relates to a radio energy transmission tuning control technology, in particular to a radio energy transmission system tuning feedback control method considering dynamic performance. Themethod includes the steps of obtaining the phase nonlinear differential equation model of the transmitting end and the receiving end of a system through analysis by utilizing a coupling mode theory and a circuit theory; utilizing a small signal linearization method to linearize a phase nonlinear differential equation model nearby a system resonance point, and analyzing the closed-loop dynamic performance of the system; taking the linear model as a controlled object and the phase value of the output voltage of an inverter circuit of the system as a reference phase, and forming a system tuning closed-loop feedback control loop by using the phase value of the transmitting end and the phase difference value of the transmitting end and the receiving end as the given values of the system transmitting end and the receiving end control loops when the system works in a resonance state. The control method can quickly and accurately control a magnetic coupling wireless energy transmission systemto work under the working states of high transmission efficiency and power, and has good robustness for detuning disturbance.
Owner:WUHAN UNIV

Generalized state space average modeling method based on aircraft electric power system dynamic characteristics

InactiveCN104915470AHas time-invariant nonlinear dynamic characteristicsGood engineering precisionSpecial data processing applicationsTransient analysisDecomposition
The invention relates to a generalized state space average modeling method based on aircraft electric power system dynamic characteristics. The method includes the steps that time-variant nonlinear differential equations of all links of an aircraft electric power system are built according to an aircraft electric power system structure; state variables are determined according to the differential equations in the above step, Fourier decomposition is conducted on the state variables, and the state variables described by the Fourier coefficients are obtained; the obtained Fourier coefficient state variables are substituted into the differential equations, and a generalized state space average model of the aircraft electric power system is obtained; the dynamic characteristics of different time scales of the aircraft electric power system are analyzed according to different flying working conditions of an aircraft; the generalized state space average model of the aircraft electric power system is simplified according to the dynamic characteristics. The generalized state space average modeling method has the advantages that by means of the method, the operating working conditions and dynamic characteristics of the aircraft electric power system can be discriminated, a time domain model can be replaced in system analysis and design, the time domain model can be simplified into the state space average model in the steady state, good engineering accuracy is achieved, fast analysis ability is achieved as well, and the generalized state space average modeling method is suitable for the field of steady state and transient state analysis of different aircraft models.
Owner:CIVIL AVIATION UNIV OF CHINA

Light unmanned aerial vehicle electrodynamic system identification method and apparatus

ActiveCN109131928AReduce adverse effectsReduced influence of pneumatic loadsAircraft components testingMathematical modelEngineering
The invention discloses a light unmanned aerial vehicle electrodynamic system identification method and apparatus, and the method includes setting up Hammerstein-type nonlinear differential equation structure of mathematical model in time domain of electrodynamic system of light unmanned aerial vehicle, including first-order linear differential element and second-order power nonlinear element, identifying linear link parameters: a photoelectric encoder disk with equal moment of inertia is used to replace the air propeller to simulate the inertia force of accelerating rotation; obtaining the time constant and amplification coefficient of the first order linear differential link from the output speed response by giving a step signal; identifying nonlinear link parameters: the nonlinear linkdoes not involve differential terms, and the nonlinear link parameters can be fitted by multiple sets of steady-state input-output relations. As that method relate to by the invention is more objective and accurate than the traditional technology, the disadvantageous influence caused by the nonlinear term generate by the aerodynamic force of the propeller can be well avoided when the differentialterm is dynamically identified; the invention uses the ground testing device, and can collect the rotational speed response on line and accurately.
Owner:CIVIL AVIATION FLIGHT UNIV OF CHINA

Energy internet communication security system and method based on chaotic system array

The invention discloses an energy internet communication security system and method based on a chaotic system array. The method comprises the following steps: 1) construction of the chaotic system array: constructing the chaotic system array with a chaotic system as a basic unit; 2) generation of a chaotic signal: solving a nonlinear differential equation of the basic unit in the chaotic system array to generate the chaotic signal required for secure communication; 3) processing of the chaotic signal: performing signal processing on the multi-channel chaotic signal generated by the chaotic array system to construct a new high-dimensional hyperchaotic signal as a key signal; and 4) encryption/decryption of information: performing encryption/decryption processing on the original/encrypted signal by using an output signal of the processed chaotic system array according to a given data encryption/decryption principle. The communication security method designed by the method provided by theinvention can be used for processing different kinds of information such as texts, waveforms, voice, images and the like, has the advantages of high data processing capability and wide type; and theenergy internet communication security system and method are flexible to expand, safe and reliable and are easy to implement.
Owner:国网河南省电力公司潢川县供电公司

Pool-type sodium-cooled fast reactor main coolant system heat transfer and flow rapid simulation method

The invention provides a pool-type sodium-cooled fast reactor main coolant system heat transfer and flow rapid simulation method, which comprises the following steps: carrying out decoupling modeling on a flow and heat transfer process of a pool-type sodium-cooled fast reactor main coolant system to realize parallelization on a simulation modeling level; removing a control body in the modeling of the flow process of the pool-type sodium-cooled fast reactor main coolant system; carrying out nonlinear equation set analytic processing on a first-order nonlinear differential equation set for describing the flow process of the pool-type sodium-cooled fast reactor main coolant system; separately solving the heat transfer process and the flow process by applying different computing resources in parallel; updating the physical parameters of each control body through the calculated pressure and enthalpy value by utilizing a physical property calculation formula; and determining whether the simulation calculation within the required time duration is completed or not. According to the method, the heat transfer and flow simulation calculation efficiency of the pool-type sodium-cooled fast reactor main coolant system is improved through decoupling modeling, control body removal in modeling, nonlinear equation set analytic processing in solving and the like.
Owner:HARBIN ENG UNIV

Calculation method of transient pressure of trapped air mass in pipe impinged by water flow

The invention provides a method for calculate transient pressure of retained air mass in pipeline impinge by water flow. The equations of motion of water column and the instantaneous equations of gaspressure are established by taking the horizontal pressurized transmission / drainage pipeline with retained air mass as the center. The second-order nonlinear differential equations are obtained by simultaneous equations with the transient flow pressure of pipeline as the strain value and the instantaneous displacement of water column as the independent variable. The equation is subjected to linearization so as to obtain the calculation formula of air-water transient pressure of retained air mass in pipeline impinge by water flow, which takes into account the effects of time, local atmosphericpressure, gas state index, water flow density, inlet pressure, pipe length, and retained air mass length. The invention provides a tool for calculation of the peak value of air-water hammer pressure and oscillation period produced by the transient flow phenomenon that the water flow impinges on a retained air mass in a pressurized pipe, and provides theoretical basis for optimizing the engineeringdesign of the pressurized transmission / drainage pipeline, reducing the engineering cost and ensuring the safe operation of the engineering calculation.
Owner:XINJIANG AGRI UNIV

A dish type solar concentrator and its design method

The invention provides a dish type solar energy concentrator. The bottom of a dish surface is provided with a circular opening, the dish surface is a rotation curved surface, and the bus of the rotation curved surface is a curve based on a specific first-order nonlinear differential equation. Disclosed is also a design method of the dish type solar energy concentrator. According to a light uniform reflection principle and related optical geometry knowledge, the specific first-order nonlinear differential equation bus equation of the rotation curved surface of the dish surface is derived through calculating. According to the dish type solar energy concentrator and the design method thereof, the dish type solar energy concentrator is provided with the dish bottom opening, and the rotation curved surface bus of the dish surface is a specific first-order nonlinear differential equation curve, so that the dish type solar energy concentrator can form quite uniform hot-fluid distribution on a receiver, and the energy conversion efficiency and other integration performance of the concentrator are substantially improved. Therefore, the dish type solar energy concentrator and the design method thereof are especially suitable for an optically focused photovoltaic solar device of a large-dimension receiver.
Owner:HUAZHONG UNIV OF SCI & TECH
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