发明名称 Departure control system using simulated phase
摘要 In the control system, a propulsion force is computed by a propulsion force computing unit based on a current command value outputted from a speed controller, an acceleration is computed by an acceleration computing unit based on the propulsion force and a running resistance outputted from a running resistance computing unit, a speed is computed by a speed computing unit based on the acceleration, and a simulated phase reference value is computed by a phase computing unit. Then, the simulated phase is computed by adding, at a simulated phase computing unit, a predetermined phase delay (e.g. 30 degrees) to the simulated phase reference value. The addition of the phase delay results in generation of synchronizing force in the LSM and thus little deviation between the simulated phase and the actual phase.
申请公布号 US6515440(B2) 申请公布日期 2003.02.04
申请号 US20010816057 申请日期 2001.03.23
申请人 CENTRAL JAPAN RAILWAY COMPANY;RAILWAY TECHNICAL RESEARCH INSTITUTE 发明人 KOGA SYUNSAKU;KITANO JUNICHI
分类号 B60L13/03;B60L15/00;(IPC1-7):H02P1/46 主分类号 B60L13/03
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