| 固体火箭发动机方案集成设计方法研究 |
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| 引用本文： | 刘金,常伯浚,沈铮铮,周济.固体火箭发动机方案集成设计方法研究[J].推进技术,1995,16(1):13-19. |
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| 作者姓名： | 刘金 常伯浚 沈铮铮 周济 |
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| 作者单位： | [1]北京精密机械总体设计院，北京100074 [2]华中理工大学， |
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| 摘 要： | 讨论了用基于知识的设计系统实现固体火箭发动机方案集成设计，论述了基于知识的设计系统的特点、结构。结合固体火箭发动机的方案设计特点，提出面向对象的知识表达方法和知识表达语言及其基于知识的设计系统的推理机制。
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| 关 键 词： | 固体推进剂 火箭发动机 方案设计 专家系统 |
AN INTEGRATED DESIGN OF THE CONCEPT OF SOLID ROCKET MOTOR |
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| Liu Jin, Chang Bojun, Shen Zhengzheng.AN INTEGRATED DESIGN OF THE CONCEPT OF SOLID ROCKET MOTOR[J].Journal of Propulsion Technology,1995,16(1):13-19. |
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| Authors: | Liu Jin Chang Bojun Shen Zhengzheng |
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| Institution: | Huazhong Univ. of Science and Technology, Wuhan, 430074;Huazhong Univ. of Science and Technology, Wuhan, 430074;Huazhong Univ. of Science and Technology, Wuhan, 430074;Huazhong Univ. of Science and Technology, Wuhan, 430074 |
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| Abstract: | n integrated concept design of solid rocket motor usingthe knowledge-based design system is discussed. The characteristics andarchitecture of the knowledge-based design system are presented. Theobject-oriented knowledge expression, the language and the reasoningmechanism of the knowledge-based design system, applied to the concept design of solid rocket motor, are given. |
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| Keywords: | Solid propellant rocket engine Tentative design Knowledge representation Knowledge base Expert system |
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