• 전력전자학회지
• /
• 제12권6호
• /
• pp.33-39
• /
• 2007

• 항공우주
• /
• 제32권
• /
• pp.33-36
• /
• 1995

• 항공우주
• /
• 제26권
• /
• pp.43-46
• /
• 1995

• 국방과기술
• /
• 4호통권182호
• /
• pp.46-57
• /
• 1994

• 국방과기술
• /
• 4호통권206호
• /
• pp.8-9
• /
• 1996

• 국방과기술
• /
• 11호통권225호
• /
• pp.17-23
• /
• 1997

• 국방과기술
• /
• 7호통권55호
• /
• pp.36-45
• /
• 1983

• 국방과기술
• /
• 5호통권183호
• /
• pp.52-59
• /
• 1994

• 전력전자학회지
• /
• 제24권4호
• /
• pp.63-69
• /
• 2019

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2009년도 추계학술대회 논문집
• /
• pp.480-485
• /
• 2009

This paper presents dynamic modeling and control analysis of a military vehicle suspension featuring MR valve structure. Firstly, the dynamic model of the suspension system which is included gas spring, MR valve and gas chamber is established with respect to the disturbance. Secondly, the friction model of the suspension system is derived by considering experiment result of the MR suspension system. And then, response characteristics of the damping force with respect to the magnetic field and friction force with the proposed friction model are provided to show the feasibility of practical application. In addition, control performance of the proposed MR suspension system is evaluated with quarter vehicle.