摘要
本文用“状态方程法”辅以Longe-Kutla数字积分法求解微分方程组,成功地进行了液压减震筒这类非线性不连续系统的时域分析。
The state-equation method in 'modern Control' has been used to simulate the dynamic responses of a hydropneumatic shock absorber of aircraft or vehicle. Based on the computer simutation, the relations between the dynamic response of the systems and the structure parameters have been revealed. Therefore, it is a successful attempt for CAD techniqhue in component design of aireraft and vehicle. The time domain analysis of a hydraulic shock absorber such kind of non-linear discontinuous system is successfully carried out, through solving differential equations with 'state equation method' and Lonqe-Kutta numerical integrity
出处
《航空学报》
EI
CAS
CSCD
北大核心
1992年第2期B098-B102,共5页
Acta Aeronautica et Astronautica Sinica
关键词
液压减震器
动态特性
计算机仿真
Hydro-pneumatic shock, Dynamic responses, Computer Simulation
