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    • 2. 发明申请
    • ZEROING METHOD USING A DISTURBANCE ESTIMATING OBSERVER
    • 使用干扰估计观察器的零点方法
    • WO1990016020A1
    • 1990-12-27
    • PCT/JP1990000721
    • 1990-06-04
    • FANUC LTDTORII, NobutoshiNIHEI, RyoKATO, TetsuakiARITA, Soichi
    • FANUC LTD
    • G05B13/04
    • G05B13/045G05B13/04
    • A zeroing method which prevents transient characteristics of a control system from being deteriorated by the provision of the observer while exhibiting the effect of removing disturbance caused by the disturbance estimating observer. Based on a practical current instruction (I-y') and a practical motor speed (v), the disturbance (x) is estimated by the disturbance estimating observer (5) equipped with four transfer elements (51 to 54) that have transfer functions (Kt/Jm, K1, K2/S, 1/S) determined by those corresponding to a torque constant (Kt) of the motor, an inertia (Jm) of the system, and parameters (K1, K2). When the positional deviation is small, an estimated disturbance is adjusted by multiplying the estimated disturbance by a feedback gain of a value ''1'' by a gain adjusting means (4), and the adjusted quantity (y') is subtracted from the current instruction (I) to remove static frictional disturbance. When the positional deviation is great, the estimated disturbance is multiplied by a feedback gain of a value ''0'' to inhibit operation of the observer, and therefore transient characteristics of the control system are prevented from being deteriorated by the operation of the observer.
    • 4. 发明申请
    • ADAPTIVE PI CONTROL METHOD
    • 自适应PI控制方法
    • WO1994002989A1
    • 1994-02-03
    • PCT/JP1993000995
    • 1993-07-16
    • FANUC LTDKATO, TetsuakiYOSHIDA, OsamuNAKAMURA, MasaruARITA, Soichi
    • FANUC LTD
    • H02P05/00
    • B25J9/163G05B2219/34448G05B2219/39178G05B2219/39181G05B2219/39194G05B2219/41123G05B2219/41425G05B2219/42037
    • This invention relates to a method of obtaining an extremely robust adaptive PI control method even when any parameter fluctuation exists in a control object. Estimation values J*, A*, Gr* and Cf* of an inertia, a coefficient of dynamic friction, gravitational disturbance due to a robot angle and Coulomb friction are determined, respectively, using (speed command r - actual speed y) as a state variable Suf, and a torque command (tau) is determined in the following way so as to make the difference between each estimation value and an actual value zero: (tau) = K2.Suf + (K1/s).Suf + J*.r' + A*.y + Gr*.sin(Theta) + Cf* + (tau)1. In this equation, the first and second terms on the right side are torque commands obtained by the PI control, r' is an acceleration of the command, (Theta) is a robot arm angle, and (tau)1 is a change-over input so as to cope with other disturbances. Since the difference between each estimation value and the actual value becomes zero, (acceleration command r = actual speed y) can be obtained and adaptative PI control having a transmission function "1" can be obtained.
    • 本发明涉及一种即使在控制对象中存在任何参数波动的情况下也能获得非常鲁棒的自适应PI控制方法。 使用(速度指令r--实际速度y)作为惯性矩,分别确定惯性的估计值J *,A *,Gr *和Cf *,动摩擦系数,机器人角度和库仑摩擦引起的重力扰动 状态变量Suf和转矩指令(τ)以下列方式确定,以使每个估计值与实际值之间的差为零:(τ)= K2.Suf +(K1 / s).Suf + J * .r'+ A * .y + Gr * .sin(Theta)+ Cf * +(tau)1。 在该等式中,右侧的第一项和第二项是通过PI控制获得的转矩指令,r'是该命令的加速度,(Theta)是机器人手臂角度,(τ)1是转换 输入,以应对其他干扰。 由于各估计值与实际值的差为零,所以能够得到(加速度指令r =实际速度y),具有发送功能“1”的适配PI控制。
    • 7. 发明申请
    • ABNORMAL LOAD DETECTING METHOD
    • 异常负载检测方法
    • WO1993008958A1
    • 1993-05-13
    • PCT/JP1992001391
    • 1992-10-27
    • FANUC LTDNIHEI, RyoNAITO, YasuoOTSUKA, KazuhisaKATO, TetsuakiSUGIYAMA, Hideki
    • FANUC LTD
    • B25J19/06
    • B25J19/06B23K11/252B25J9/1674
    • A method of accurately detecting the abnormality of a load, such as the fusion at a free end of a spot gun. In this load abnormality detecting method, while a flag F2 which is set to ''1'' when an instruction for moving a movable mechanical part is outputted, and which is reset to ''0'' after a predetermined very short period of time has then elapsed, is in ''0'' because the movable part is stopped, estimated disturbance torque T0 is first determined successively by a disturbance estimating observer, updated and stored (S4, S11). When an instruction for moving the movable mechanical part is outputted and the flag F2 is set to ''1'', an estimated disturbance torque T1 is determined (S5). When an absolute value [T1-T0] of the difference between this torque T1 and estimated disturbance torque T1 determined immediately before the starting of the movable mechanical part exceeds a reference level Ts (S6), an alarm representing the occurence of a load abnormality is given (S7), and a flag F1 is set to ''1'' to stop the operation (S3, S8). The estimated disturbance torque T0 during the stoppage of the movable mechanical part represents a value such as the gravity which this part receives during this time. Consequently, the value, [T1-T0] represents the disturbance torque, from which the influence of gravity is eliminated, during the movement of the mechanical part. By comparing this value with the reference value Ts, a force exerted on the movable part, other than the gravity and a frictional force, can be detected more accurately. Therefore, abnormality, such as the occurrence of fusion can be determined accurately.