推进技术 ›› 1996, Vol. 17 ›› Issue (5): 14-17.
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陆曙军,张育林
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摘要： 建立了液体火箭发动机的降阶非线性动态模型。针对已发生过的或极有可能发生的故障形式，进行了故障状态下动态特性模拟。仿真结果表明，所建模型较精确合理，并能实现实时随机仿真。
关键词: 液体推进剂火箭发动机;发动机故障;故障分析;实时模拟
Abstract: resent a reduce-order nonlinear dynamic model of a liquid rocket engine.For everykind of fault types,dynamic simulation under condition of fault has been carried out.The resultsindicate that top model is reasonable and accurate,and real-time random simulation is achieved.
Key words: Liquid propellant rocket Engine;Engine failure;Fault analysis;Real timesimulation
陆曙军,张育林. 液体火箭发动机故障实时仿真模型[J]. 推进技术, 1996, 17(5): 14-17.
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