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47results about How to "Suppress residual vibration" patented technology

Method for controlling index time-varying slide mode of flexible spacecraft characteristic shaft attitude maneuver

ActiveCN103412491ASuppress residual vibrationAvoid complex coupling relationshipsAdaptive controlDynamic modelsSpace vehicle control
The invention relates to a method for controlling an index time-varying slide mode of flexible spacecraft characteristic shaft attitude maneuver, and belongs to the technical field of spacecraft control. The method comprises the steps that firstly, a system dynamically equivalent model, a dynamic model and a flexible vibration model are established under a spacecraft system, then, the vibration frequency and the damping ratio parameter of a closed loop system with the index time-varying slide mode control law are calculated, and a single-shaft multi-modality filtering input shaping device with a characteristic shaft as a rotary shaft is designed according to the designing method of the single-shaft input shaping device to restrain flexible vibration in three-shaft motion. Meanwhile, a state observer is designed to estimate flexible modal information in real time, and the method for controlling an output feedback index time-varying slide mode is formed. At last, saturability analysis is conducted on control torque so as to satisfy the physical saturation constraint of the control torque. By means of the method, the application range of existing input shaping is expanded, the input shaping technology is expanded from single-shaft maneuver to three-shaft maneuver, the self-robustness of filter input shaping is enhanced, and the purpose that the attitude maneuver path of the spacecraft is the shortest is achieved.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Testing device and method for residual oscillation restraining of flexible joint-flexible arm system

The invention discloses a testing device for residual oscillation restraining of a flexible joint-flexible arm system. The testing device for the residual oscillation restraining of the flexible joint-flexible arm system comprises a data processing module, a drive module, a mechanical system module and a signal acquiring module. The data processing module adopts an industrial personal computer andcomprises a man-machine interaction unit and a real-time control unit. The drive module comprises an alternating current servo driver and an alternating current servo motor. The mechanical system module comprises a supporting base, a system pedestal, a flexible joint and a flexible arm. The signal acquiring module comprises a three-dimensional acceleration sensor, a switching power source and a data acquisition unit, and the three-dimensional acceleration sensor is arranged at the tail end of the flexible arm. The invention further provides a method for residual oscillation restraining of theflexible joint-flexible arm system. By means of the testing device and method, the main oscillation modal parameters of the flexible joint-flexible arm system can be rapidly acquired, the problem that system model parameters are not matched, and consequently an input reshaper is not reasonable in design is solved, the residual oscillation of the mechanical system is effectively restrained, and rapid and accurate positioning of a mechanism arm is achieved.
Owner:SOUTH CHINA UNIV OF TECH

Input shaping residual vibration suppression method and system adapting to trajectory errors of motion system

The invention provides an input shaping residual vibration suppression method adapting to trajectory errors of a motion system, comprising the following steps: S1, acquiring the inherent frequency anddamping coefficient of a mechanical system; S2, establishing a mathematical model about a linear programming problem of pulse amplitude parameters of an input shaper, and acquiring a pulse amplitudeexpression of the input shaper; S3, performing convolution operation on an input signal for reference and a pulse signal of the input shaper to obtain a shaped command curve C1; S4, using the C1 curvein the S3 to drive the system to obtain an actual motion trajectory curve P1 and a trajectory error curve C1-P1 under the current motion form; S5, using the C1-P1 curve to compensate the curve C1 toobtain a next command curve C2, using the curve C2 to drive the system to obtain a trajectory error curve C1-P2 under the current motion form, and using C1-P2 to compensate C2 to obtain a next commandcurve P3; and S6, repeating S5 to use the trajectory error curves C1-P1, 2,...n to compensate the command curves P1, 2,...n to obtain a next command curve until the value of the trajectory error curve at each moment is close to zero. According to the method for suppressing residual vibration through the input shaper, other hardware equipment does not need to be added, and cost is saved.
Owner:SHENZHEN COLIBRI TECH

Liquid ejecting apparatus and control method of the same

A liquid ejecting apparatus includes a liquid ejecting head having a nozzle, a pressurizing chamber that communicates with the nozzle, and a pressurizing element that causes a pressure change in liquid within the pressurizing chamber, the liquid ejecting head being capable of ejecting liquid from the nozzle by operating the pressurizing element; and a driving signal generation unit that generates a driving signal including a driving pulse that drives the pressurizing element. The driving signal includes an ejection driving pulse that ejects a liquid droplet and a non-ejection driving pulse that drives the pressurizing element to a degree whereby a liquid droplet is not ejected. The ejection driving pulse is a pulse waveform having an expansion element that causes the pressurizing chamber to expand and retract a meniscus toward the pressurizing chamber and a constriction element that causes the pressurizing chamber expanded by the expansion element to constrict and push the meniscus in the direction of ejection. The non-ejection driving pulse is a pulse waveform having an expansion element that causes the pressurizing chamber to expand and retract the meniscus toward the pressurizing chamber, a holding element that holds the voltage at the end of the expansion element for a set amount of time, and a constriction element that causes the pressurizing chamber expanded by the expansion element to constrict and push the meniscus in the direction of ejection. When the length of time from the end of the constriction element in the ejection driving pulse to the beginning of the expansion element in the non-ejection driving pulse is taken as t, the lengths of time of the expansion element, holding element, and constriction element in the non-ejection driving pulse are taken as a, b, and c, respectively, and the inherent vibration cycle of the liquid within the pressurizing chamber is taken as Tc, t, a, b, and c are within the ranges defined by the following equations (1) through (3):
Tc/4≦t≦Tc/2  (1)
(5Tc/8)−t≦a≦(3Tc/4)−t  (2)
b+c=Tc−t−a  (3)
Owner:SEIKO EPSON CORP

Vibration control method for rigid-flexible coupling electromechanical servo system

The invention discloses a vibration control method for a rigid-flexible coupling electromechanical servo system. The vibration control method comprises the steps of separately collecting encoder dataon a drive motor and a load motor, acquiring torsion angles of two ends of a flexible shaft rod, computing the torsion angle of a micro unit located at any position of the flexible shaft rod, and computing a frequency domain characteristic equation according to the length, polar moment of inertia, elasticity modulus and rotational inertia of the flexible shaft rod; by using the frequency domain characteristic equation, computing a coupling torque between the flexible shaft rod and a rigid driving flywheel; building a rigid driving flywheel balance equation; putting the coupling torque into thebalance equation to acquire a frictional order transfer function model of the system; and according to the frictional order transfer function model, building a fractional order controller, and controlling the vibration of the system by using the controller. According to the method provided by the invention, the dynamic behaviors of the viscous-elastic material is accurately described via the frictional order model, and the residual vibration of the system is effectively suppressed.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Servo system residual vibration suppression method based on parameterized feedforward

The invention discloses a servo system residual vibration suppression method based on parameterized feedforward, and belongs to the technical field of mechanical equipment control. The invention discloses a servo system residual vibration suppression method based on parameterized feedforward, which comprises the following steps of: calculating a feedforward force through an input track and a parameterized feedforward controller by utilizing a primary function parameterized feedforward controller; introducing a performance objective function of a parameterized feed-forward control algorithm according to an optimal control theory to identify parameters of the input shaping filter and the feed-forward controller; analyzing the error of the parameterized feedforward control and the convergence of the identification parameters; and solving the optimal value of each parameter. Through continuous exploration and test, a parameterized feed-forward control algorithm is adopted, the control difficulty of the servo system can be effectively reduced, the calculated amount of a processor is reduced, the flexibility is high, the operation speed is high, the robustness is good, the control effect is good, and the control requirement of the servo system can be met.
Owner:ZHEJIANG SCI-TECH UNIV

A Vibration Control Method of Rigid-Flexible Electromechanical Servo System

The invention discloses a vibration control method of a rigid-flexible coupling electromechanical servo system, comprising: separately collecting encoder data on a drive motor and a load motor, obtaining the torsion angles at both ends of a flexible shaft in real time, and calculating the flexible shaft The torsion angle of the micro-element at any position on the above is calculated according to the length, polar moment of inertia, elastic modulus and moment of inertia of the flexible shaft to obtain the frequency domain characteristic equation; using the frequency domain characteristic equation to calculate the described The coupling torque between the flexible shaft and the rigid drive flywheel; the balance equation of the rigid drive flywheel is established; the coupling torque is brought into the balance equation to obtain the fractional transfer function model of the system; according to the fractional transfer function model, establish a fractional order controller, and use the controller to control the vibration of the system. The method involved in this patent accurately describes the dynamic behavior of the viscoelastic material through the fractional order model, and effectively suppresses the residual vibration of the system.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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