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259 results about "Maximal acceleration" patented technology

S-shaped acceleration and deceleration control method for changing speed and position of object on line

ActiveCN106168790AAcceleration curve continuousNo mutationNumerical controlDiscretizationPlanning method
The present invention provides an S-shaped acceleration and deceleration control method for changing speed and position of an object on line. The method comprises the acceleration phase speed planning, the deceleration phase speed planning, the constant speed phase speed planning, the real speed reduction point predication, the maximum speed processing, the surplus distance compensation, the online object speed changing algorithm and the online object position changing algorithm. An acceleration and deceleration discretization speed planning method is employed and the user input parameters are combined to calculate the operation time of a seven-phase speed planning phase. It is determined whether the maximum acceleration and the maximum speed can reach the criterion or not, the integration problem of a sampling period Ts according to the acceleration/deceleration acceleration, the acceleration/deceleration speed and the final position L after discretization is considered, and the real reachable acceleration/deceleration acceleration, the acceleration/deceleration speed and the feed rate are corrected. The S-shaped acceleration and deceleration control method for changing speed and position of the object on line greatly simplifies an original calculation formula and saves lots of operation time of a computer, and the surplus distance employs a one-time compensation method in the speed reduction process.
Owner:SOUTH CHINA UNIV OF TECH

Speed look-ahead control method based on filter technique

ActiveCN101470434AAvoid unbearable shocksWith flexible adaptive control capabilityProgramme controlComputer controlEngineeringContour error
The invention relates to a look-ahead velocity control method based on filtering technique, which comprises steps of linking path segments of a processing curve into a path chain, prospectively calculating a constraint velocity for a maximum acceleration and a constraint velocity for the profile error at the corner of the processing curve, operating the corner velocity according to each constraint velocity, prospectively planning the integral velocity of the path chain through the linear accelerating and decelerating strategy to obtain a prospectively planned velocity of the path chain, and utilizing a differential value between the corner velocity and the path chain prospectively planned velocity as a criterion to judge whether decelerating in advance or not during the interpolation procedure, if the differential value is out of a stated threshold value, then calculating the length of the decelerating segments in the path chain, reversely recursing the decelerating path segments in the path chain to set the required feeding velocity, performing track planning to the path chain , and realizing self-adaptive adjustment of the processing velocity along with geometric configuration changes of processing paths through adjusting the required feeding velocity of the decelerating path segments. The look-ahead velocity control method has the advantages of high flexible self-adapting control capacity, high executing efficiency, good velocity smoothness and the like.
Owner:SHENYANG GOLDING NC & INTELLIGENCE TECH CO LTD

Unmanned aerial vehicle auxiliary wireless sensor network and node scheduling and flight parameter design method thereof

The invention discloses an unmanned aerial vehicle auxiliary wireless sensor network and node scheduling and flight parameter design method thereof, and belongs to the wireless technical field of thewireless communication and internet of things. The unmanned aerial vehicle auxiliary wireless sensor network comprises an unmanned aerial vehicle air base station and K single-antenna ground terminalnodes; the unmanned aerial vehicle air base station performs movement according to an optimized path, speed and acceleration and like flight parameters at the specified flight time; at each flight moment, the unmanned aerial vehicle base station sends data to a scheduled ground terminal node, and only communicates with one terminal node at each moment. Through the method disclosed by the invention, the system energy efficiency maximization is used as the target, and a terminal node scheduling policy and unmanned aerial vehicle flight path, the flight speed and the acceleration are used as theoptimization variable, so that a mathematical model is established in consideration of the unmanned aerial vehicle maximum flight speed, the maximum acceleration and the uniform acceleration, the terminal node data transmission rate fairness and like conditions, thereby solving to obtain a suboptimal terminal node scheduling and unmanned aerial vehicle parameter solution.
Owner:ZHENGZHOU UNIVERSITY OF AERONAUTICS

Gait identity identification method based on mobile phone acceleration sensor and system thereof

The invention discloses a gait identity identification method based on a mobile phone acceleration sensor and a system thereof. The method comprises the following steps of using a mobile phone acceleration sensor to collect gait data of a person to be measured in a section of journey; preprocessing the acquired gait data, carrying out linearity interpolation and filtering on triaxial acceleration signals x, y and z, and then synthesizing a resultant accelerated speed; carrying out period segmentation on a synthesized resultant accelerated speed sequence, using a DTW algorithm to filter a period, and filtering a disqualification period and acquiring a qualified period; extracting time domain and frequency domain characteristics from the qualified period, wherein the time domain characteristic includes 8 characteristics of an z-axis-direction average maximum acceleration speed, an average minimum acceleration speed, an average acceleration speed, a root mean square, a standard deviation, a peak value factor, kurtosis and an average absolute difference, and the frequency domain characteristic includes first five coefficients of FFT conversion and first five coefficients of DCT conversion so that 18 dimension characteristics are formed; and using a classifier which is trained in advance to identify the 18 dimension characteristics of the person to be measured.
Owner:WUHAN UNIV OF TECH

Mechanical type automatic transmission gear shifting method

The invention relates to a mechanical type automatic transmission gear shifting method. The mechanical type automatic transmission gear shifting method includes the following steps that the current vehicle mass and the current slope are acquired; with the maximum acceleration which a vehicle can reach as a power performance index, a best power performance gear position under different vehicle speeds, different accelerations, different accelerator opening degrees, different masses and different slopes is calculated, and serves as a vehicle power performance gear shifting strategy; with the motor efficiency being an economic index, on the basis that the slope climbing requirement of the vehicle is met, a best economy gear position under different vehicle speeds, different accelerations, different accelerator opening degrees, different masses and different slopes is calculated, and serves as a vehicle economy gear shifting strategy; and the current power performance and economy requirements of the vehicle are judged, one of the vehicle power performance gear shifting strategy and the vehicle economy gear shifting strategy is selected to determine a gear shifting point. For different masses of the vehicle and different slopes of a road, an optimal gear shifting strategy is calculated; by means of a multi-target optimization method based on road condition information and a vehicle state, the gear shifting strategies are optimized, so that the intelligent level of gear shifting can be improved, frequent gear shifting is avoided, and power performance and economy of the vehicle become best.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Time optimal rapid three-dimensional obstacle avoidance path planning method

ActiveCN109828600ARealize online planningImprove task responsivenessPosition/course control in three dimensionsOptimal controlSimulation
The invention discloses a time optimal rapid three-dimensional obstacle avoidance path planning method, particularly relates to an unmanned aerial vehicle obstacle avoidance path planning method, andbelongs to the field of unmanned aerial vehicle path planning. According to the invention, the method comprises the steps: establishing an unmanned optimal control model which takes the acceleration in each direction as a control variable and contains the flight time sum through considering the maximum acceleration and obstacle constraint conditions; loosening an original non-convex nonlinear optimization problem into a second-order cone programming problem; and finally, solving a series of second-order cone programming problems through iteration to obtain a solution of an original problem andobtain an optimal change strategy in the speed direction. In other words, the obstacle avoidance path planning with the optimal time is realized by coordinating the flight time and the flight speed direction, the online planning of the obstacle avoidance path and the related control quantity can be realized, and the task response capability of the unmanned aerial vehicle can be further improved through the optimized flight path with the optimal time.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Improved self-disturbance-resistance quad-rotor unmanned aerial vehicle height control method

ActiveCN109839822AOvercoming the problem of insufficient anti-interference abilityImprove immunityControllers with particular characteristicsDifferentiatorDynamic models
The invention discloses an improved self-disturbance-resistance quad-rotor unmanned aerial vehicle height control method. The method comprises the following steps of step1, based on a mechanism modeling method, establishing a nonlinear dynamic model of a quad-rotor unmanned aerial vehicle height direction; step2, decomposing the nonlinear dynamic model into a linear item and a uncertain item; step3, using a tracking differentiator to obtain a height direction position and a speed expectation value; step4, estimating a disturbance item in a system using a first-order extended state observer; and step5, designing an error feedback control law based on a PD algorithm and feedforward control, and using a disturbance item value estimated by the extended state observer to compensate the uncertain item of the system. An improved tracking differentiator is used to plan a height flight strategy, and an acceleration-uniform speed-deceleration flight mode is constructed so that a quad-rotor unmanned aerial vehicle can rise (or descend) from one height to another height in the shortest time; and a maximum acceleration during flight and a speed of a uniform speed segment can be set autonomously.
Owner:中国人民解放军火箭军工程大学

Non-sinusoidal vibration method for continuous casting crystallizer

InactiveCN103752783AGood waveform dynamicsConstant accelerationSinusoidal vibrationMaterials science
The invention discloses a non-sinusoidal vibration method for a continuous casting crystallizer. According to the technical scheme, the non-sinusoidal vibration method for the continuous casting crystallizer comprises controlling a driving device of the continuous casting crystallizer to enable the continuous casting crystallizer to perform non-sinusoidal vibration according to speed waveforms which are confirmed according to following functions in every vibration period with the driving of the driving device; enabling the vibrating process of every vibration period to be formed by seven sections; enabling the crystallizer to move according to a given vibrating method due to control of the driving device of the crystallizer and achieving the non-sinusoidal vibration. The non-sinusoidal vibration method for the continuous casting crystallizer has the advantages of being smooth and continuous in displacement and speed waveform, having no mutation in accelerated speed, not generating rigid and flexible impact and having good waveform dynamic characteristics and enabling the largest accelerated speed of the movement of the crystallizer to be served as a quantity which is reflected in the waveforms, enabling the quantity to be allowed setting according to actual conditions and to be invariant, increasing waveform deflection rate, enabling non-sinusoidal vibration of the crystallizer to be enhanced but the accelerated speed of the vibration of the crystallizer to be kept constant and guaranteeing movement smoothness of the crystallizer.
Owner:YANSHAN UNIV

Spline curve interpolation algorithm for high quality processing

The invention discloses a spline curve interpolation algorithm for high quality processing, and the spline curve interpolation algorithm for high quality processing comprises the following steps: quickly pre-interpolating the numerical control machining curve, recording the length of the interpolation path and the maximum/minimum value of the acceleration/deceleration process; calculating the maximum acceleration and most much acceleration of the acceleration/deceleration process, having subsection on the acceleration/deceleration process, calculating quadratic polynomial speed equations of each section; obtaining the speed equation according to the pre-interpolating stage at the real time interpolating stage, adopting the strategy that the theory chord length is close to the practical chord length for building the construction function, estimating the initial value of the interpolation parameter and building the parabolic interpolation polynomial, using the Newton iteration method for exactly calculating the interpolation parameter. The speed plan adopts five-section S curve acceleration/deceleration control algorithm for guaranteeing continuous change of the speed and accelerated speed, the bounded change of the accelerated acceleration speed and the running stability of the machine tool; the calculation of the interpolation parameter adopts the combination of parabolic interpolation method and Newton iteration method for controlling the feeding speed fluctuation of the real time interpolation in the ideal level and satisfying the high quality processing requirement.
Owner:中国科学院沈阳计算技术研究所有限公司

Method for evaluating overall earthquake damage level of reinforced concrete frame structure based on equivalent single-degree-of-freedom system

The invention relates to the technical field of earthquake damage evaluation, in particular to a method for evaluating the overall earthquake damage level of a reinforced concrete frame structure based on an equivalent single-degree-of-freedom system. The method is used for quickly and accurately evaluating the overall earthquake damage level of the structure after an earthquake by using strong ground motion data acquired by the structure. The method includes the steps that a multi-degree-of-freedom system structure is equivalent to the single-degree-of-freedom system structure, and namely the multi-degree-of-freedom system with N layers is equivalent to the single-degree-of-freedom system, wherein the mass M[e] of the single-degree-of-freedom system is equal to the total mass of the multi-degree-of-freedom system; the maximum acceleration response of the equivalent single-degree-of-freedom system under the same earthquake ground motion effect is worked out; the ductility coefficient of the equivalent single-degree-of-freedom system under the same earthquake ground motion effect is worked out; damage index calculation is carried out; structural damage evaluation is carried out. By means of the method, the defects that large errors can be caused in a damage evaluation method based on modal parameters and time and labor are consumed and results are prone to divergence in a damage evaluation method based on physical parameters are overcome, and the overall earthquake damage level of the structure can be easily, quickly and effectively evaluated in a quantitative mode.
Owner:INST OF ENG MECHANICS CHINA EARTHQUAKE ADMINISTRATION

Space robot jitter suppression trajectory planning method based on accelerated speed dynamic configuration

InactiveCN103970019ASolving residual jitter problemsSolve the problem of variable frequency track jitterAdaptive controlRobotic systemsKinematics
The invention discloses a space robot jitter suppression trajectory planning method based on accelerated speed dynamic configuration, and belongs to the technical field of robot jitter suppression. The method aims at solving the problems that an existing robot system is prone to residual jitter, tracing accuracy is not high, and a robot can not be accurately positioned; the robot is not stable in the operation process; task execution time of the robot is prolonged due to time delay; the calculated amount is large, and the requirement for operational capacity of a controller of the robot is high. The method includes the steps that the minimum execution cycle of a trajectory section is estimated according to input expected displacement and the maximum accelerated speed limit; a finial trajectory cycle is determined according to the calculated minimum execution cycle and a given trajectory cycle; a minimum-order jitter cycle, of a robot system, determined at an initial joint angle is calculated according to kinetic and dynamic parameters of the robot and robot joint rigidity parameters; a corresponding trajectory planning method is selected according to the trajectory cycle, accelerated speed time and the jitter cycle. The method is suitable for the field of robot jitter suppression.
Owner:HARBIN INST OF TECH

Akima spline fitting based look-ahead interpolation method

The invention provides an Akima spline fitting based look-ahead interpolation method. The method is characterized in that the Akima spline fitting is that the parameters corresponding to each interpolation point are calculated by the centripetal parameterization method, and then the data points are fitted into a smooth Akima spline by the Akima five-point interpolation method; the look-ahead interpolation is that different values are returned for real-time interpolation by the look-ahead interpolation calculation according to the processing precision requirement, the programming speed of a numerical control system and the maximum speed information; the real-time interpolation is that the real-time feeding speed is adjusted according to the look-ahead interpolation returning value, then a structural equation is created according to the known Akima spline equation and interpolation cycle and other information, then the primary iteration value of the next interpolation method is predicated, and finally the interpolation parameters are accurately calculated by the newton iteration method. According to the method, the data points to be processed are fitted through the Akima spline, so that the actuating efficiency is increased, the smoothness is high, the fitting precision is improved while the interpolation real-time performance is ensured, the accuracy and flexibility are improved, and the actual state of a workpiece can be restored to the maximum.
Owner:中国科学院沈阳计算技术研究所有限公司
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