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yi zhong qi ti jian ya qi dong tai wei fen fang cheng de tui dao
Author(s): 
Pages: 52-60
Year: Issue:  4
Journal: Aerospace Control

Keyword:  气动系统减压器微分方程;
Abstract: 本文针对卫星控制系统喷气执行机构中的气体减压器输出流量变化而引起减压器振荡的问题,讨论了减压器各部分的线性化微分方程、气体状态微分方程、质量系统的运动方程,并推导出减压器运动方程。
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