2002
DOI: 10.1243/095440702762508236
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System dynamic modelling and adaptive optimal control for automatic clutch engagement of vehicles

Abstract: A non-linear multi-rigid-body system dynamic modelling is developed for the automated clutch system in power transmission during clutch engagements, especially at sharp vehicle start-up, sudden engine flame-out, low driving speed and clutch plate overwearing. In order to guarantee an ideal dynamic performance of the clutch engagement, an adaptive optimal controller is designed by considering throttle angle, engine speed, gear ratio, vehicle acceleration and road condition. A non-linear model reference adaptive… Show more

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Cited by 44 publications
(46 citation statements)
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“…where engine output torque Me as the driving torque in the clutched train system is function in literature by Zhang et al (2002); referring to Inalpolat & Kahraman's study (2008), transmission error excitation e Sj,Pji (j=1,2) and e Rj,Pji (j=1,2) are defined in Fourier series form based on evaluation of overall effective mesh stiffness fluctuations; relative gear mesh displacements are defined as δ Sj,Pji =r Sj ·(θ Sj -θ A )+r Pj ·(θ Pji,A -θ A ), δ Rj,Pji =r Rj ·(θ Rj -θ A )-r Pj ·(θ Pji,A -θ A ) and δ R1,G =r R1 ·θ R1 ; relative displacement θ Pji,A of planet P ji (j=1,2) to arm is defined as θ Pji,A =θ Pji -θ A ; total inertia J A ' of the arm with (n1+n2) planets is defined as J A '=J A +n1·J P1 +n2·J P2 +n1·m P1 ·(r S1 +r P1 )+n2·m P2 ·(r S2 +r P2 ) where J A is moment of inertia of the arm; m P is mass of a planet; and n1 and n2 are number of planets of PGS-I and PGS-II, respectively. Similarly, equations of motion for PGS-II are described as: ( 2 2 2 2 , 2 2 , 2 2 2 , 2 2 2 2 2 , 2 2 , 2 2 2 , 2 2 ( , 2 2 , 2 2 1 2 , 2 2 2 , 2 , 2 2 , 2 2 1 2 , 2 2 2 , 2 2 …”
Section: Dynamicsmentioning
confidence: 99%
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“…where engine output torque Me as the driving torque in the clutched train system is function in literature by Zhang et al (2002); referring to Inalpolat & Kahraman's study (2008), transmission error excitation e Sj,Pji (j=1,2) and e Rj,Pji (j=1,2) are defined in Fourier series form based on evaluation of overall effective mesh stiffness fluctuations; relative gear mesh displacements are defined as δ Sj,Pji =r Sj ·(θ Sj -θ A )+r Pj ·(θ Pji,A -θ A ), δ Rj,Pji =r Rj ·(θ Rj -θ A )-r Pj ·(θ Pji,A -θ A ) and δ R1,G =r R1 ·θ R1 ; relative displacement θ Pji,A of planet P ji (j=1,2) to arm is defined as θ Pji,A =θ Pji -θ A ; total inertia J A ' of the arm with (n1+n2) planets is defined as J A '=J A +n1·J P1 +n2·J P2 +n1·m P1 ·(r S1 +r P1 )+n2·m P2 ·(r S2 +r P2 ) where J A is moment of inertia of the arm; m P is mass of a planet; and n1 and n2 are number of planets of PGS-I and PGS-II, respectively. Similarly, equations of motion for PGS-II are described as: ( 2 2 2 2 , 2 2 , 2 2 2 , 2 2 2 2 2 , 2 2 , 2 2 2 , 2 2 ( , 2 2 , 2 2 1 2 , 2 2 2 , 2 , 2 2 , 2 2 1 2 , 2 2 2 , 2 2 …”
Section: Dynamicsmentioning
confidence: 99%
“…where relative gear mesh displacements are defined as δ R2,P =r R2 ·θ R2 +r P ·θ P and δ M,G =r M ·θ M ; ∆p is the pressure drop between the reversible motor-pump inlet and outlet ports; D v is the displacement of reversible motor-pump; ƞ m is the mechanical efficiency of reversible motor-pump; and function of vehicle resistant torque M r refers to literature by Zhang et al (2002).…”
Section: Dynamicsmentioning
confidence: 99%
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