英语翻译Experimental results for the magnetic coupling can be seenin Fig.10 where both the load disturbance and torsion angleerrors are corrected for a load-side set-point position-referenced system.Although the results shown in Fig.10 show fast

来源:学生作业帮助网 编辑:作业帮 时间:2024/04/30 00:31:01
英语翻译Experimental results for the magnetic coupling can be seenin Fig.10 where both the load disturbance and torsion angleerrors are corrected for a load-side set-point position-referenced system.Although the results shown in Fig.10 show fast
xWMs+oiWc;uǝӴһN hA@+Qe$[vH,K\rEUB}Avɲ3Z{{=*߆}V~uQwny)-+mGxy] KڥiX"Y" W-_d^wteZN +9Br³װ-}݂fF*zE=I{}2! M {\}](hDjj{IOio:Զ;]QsSV0n-BѱA1L$M!#ե#vIE0,*Nm'pSb8vm/j≂aRavruQ>)@0i@mkH@"t.T iO"ޫWxeD^3I rF˫z!P kJ垞[[~@/.J9g/蘅+ٯ~y_`'(4/9800ş ϗR/HHQz[w$^ ۂVHpSt4wu4̕ Vn)-Zl< -7 VZUyCYJ P1z,C"T6x-hiV60âM[jbxZjFLRSq(*\Í:H; |.eLiE c"s3p}|  6g 4ҫJP* Nþv n'l xΜ*8nɠG8LVXt MAc5&gSC!>~~Ų^3yw~7qZ9!g\.0 doޤ=_9J6Txth1ĝhCtx9S?ZK ؔ/&pLܩ+>-޾owWjpTVp?jx<ۼz 7/ɧG nXLj9w ,p]]kNѩ;C^bxyN pzAνDN?zsi:,"A[p_ vdb4Ճx*.ֱl=\̬,j-"A| GƏː#xDj`䑋sxY-<$-jr11W52?=zBb?s+5F܀ڪ"#_۷` poY+Acd=!pYy<KypOAjY=I'ynw<;Hhln,셼wlggs)A.ɭO# )jTA;^} %[3'6.

英语翻译Experimental results for the magnetic coupling can be seenin Fig.10 where both the load disturbance and torsion angleerrors are corrected for a load-side set-point position-referenced system.Although the results shown in Fig.10 show fast
英语翻译
Experimental results for the magnetic coupling can be seen
in Fig.10 where both the load disturbance and torsion angle
errors are corrected for a load-side set-point position-
referenced system.
Although the results shown in Fig.10 show fast disturbance
rejection and torsion angle compensation,noticeable deviation
occurs on the load-side position.The small variations in load-
side position are owing to the somewhat poor integrity of the estimated load torque,a consequence of too fast observer
dynamics.To improve load-side position stability,the
estimates of load-side position and disturbance torque are
constructed from separate minimum-order observers,a ‘fast’
observer for load-side position with observer poles placed as
previously,and a ‘slow’ observer for load-torque estimation
with observer poles placed at half the ‘bandwidth’ of the fast observer.This enhanced technique is referred to as the
dual-observer method and the modified controller structure is
shown in Fig.11 [12].
The separation of the disturbance torque estimate and the
load-position estimate into slow and fast observers,
respectively,produces a substantial improvement in load-
side set-point position tracking.Fig.12 illustrates the results
for this enhanced dual-observer-based controller strategy.
The performance of the experimental system incorporating
the dual-observer approach is outstanding as can be seen from
Fig.12.Both steady-state disturbance and torsion angle error
have been compensated providing perfect load-side set-point
position tracking.However,this is at the expense of
somewhat slower response.
5 Load angle observation error and
correction
For load-side disturbance torques up to approximately 50% of
the rated pull out torque the magnetic coupling behaves
entirely linearly.However,for a disturbance torque .50%,
the coupling’s torque transfer increasingly deviates from the
linear approximation.As the load-side position is estimated
from a linear observer,at high disturbance torque the
estimated load-side position and true load-side position
begin to deviate.To illustrate the non-linearity error
inherent in an observer constructed from a linear model,
consider the simulation results of Fig.13 with a reference
position of 0 radians and disturbance of 75% of rated
torque TG.
The observed load-side position differs from the true
position because the state estimation is constructed from a
linearised two-inertia model.Consequently,a modification
of the load-side position estimate is necessary.In steady-
state,the linear load-side position estimate is given by………………

英语翻译Experimental results for the magnetic coupling can be seenin Fig.10 where both the load disturbance and torsion angleerrors are corrected for a load-side set-point position-referenced system.Although the results shown in Fig.10 show fast
对于电磁联结器的实验结果能被预期
在图 10 哪里两者的装载扰动和扭转角
错误为一个装载-边的决胜点职务被修正-
叁考的系统.
虽然在图 10 被显示的结果表示快速的扰动
拒绝和扭转按某一角度转动补偿,引人注目的误差
在装载-边的职务上发生.装载中的小变化-
旁的职务由于估计装载扭矩的有一些贫穷正直,太快速观察者的结果
动力学.要改良装载-边的职务稳定这
装载-边职务和扰动扭矩的财测是
从分开的最低定货观察者装配,一 " 斋戒 "
观察者为装载-边的职务用观察者极放置当做
先前,和一位 " 缓慢的 " 观察者为装载-扭矩的判断
与观察者极放置在快速观察者的一半的’频宽’.这个可提高的技术被称为这
双重观察者方法和 modi?ed 会计长结构是
在图 11[12] 显示.
扰动的使解除契约扭矩估计和这
装载-职务估计进入缓慢、快速的观察者之内,
分别地,在装载中生产一个可观的改良-
边决胜点放置追踪.图 12 举例说明结果
为这提高了双重-以观察者为主的会计长战略.
实验系统合并的运转
双重观察者方法是未解决的因为能被预期从
图 12.不变的扰动和扭转按某一角度转动错误
已经被补整提供完全的装载-边的决胜点
放置追踪.然而,这是牺牲
有一些较慢的回应.
5装载角观察错误和
修正
因为装载-边的扰动扭矩提高到大约 50%
定格者拉出扭矩,电磁联结器举止
完全地线性地.然而,为扰动扭矩 .50%,
联结器扭矩转帐逐渐地脱离这
线型的近似值.当做装载-边的职务正在估计
从一位线性的观察者,在高度扰动扭矩这
估计装载-边的职务和真实的装载-边职务
开始脱离.举例说明非直线性的错误
在一位观察者的固有的从一个线性的模型装配,
用一个叁考考虑图 13 的模拟结果
0个弧度的职务和扰动 75% 定格的
扭矩 TG.
被观察的装载-边的职务差异从这真实的
因为规定判断构成,所以放置一
被使线性化的两惯性的模型.结果,modi?阳离子
装载-边职务估计是必需的.在定态中-
规定,线性的装载-边的职务估计有在…之前……………