再入飞行器气动布局优化设计是一个复杂的工程系统设计问题，通常包含若干子系统和大量的设计参数。
The optimization design of aerodynamic shape for reentry vehicles (ASRV) is a design problem of the complex engineering system, which often involves several subsystems and various parameters.
各控制子系统的设计采用自适应控制和神经网络相结合的方法，所提出的参数和权重的自适应调整律保证系统的稳定性。
Each subsystem is designed using adaptive control with neural network compensation. The stability of the system is guaranteed by the proposed parameter and weight turning law.
此方法同样可用于仪器仪表、机械及电子系统参数的优化设计。
The method may also be used in parameters optimization of mechanical and electronic system and in optimal design of instruments.
设计参数合理的外弹性阻尼支承可以明显改善轴承-转子系统的固有特性及强迫振动响应。
External elastic damping support, if designed reasonably, may obviously improve the natural or forced vibration response characteristics of bearing rotor systems.
设计了风机转子系统参数化有限元建模，并在通用商业化有限元分析软件ALGOR基础上，开发了模块化编程。
The finite element model of fan rotor system parameterization is designed. Modularity programming is developed based on general business finite element analyzing software ALGOR.
设计了风机转子系统参数化有限元建模，并在通用商业化有限元分析软件ALGOR基础上，开发了模块化编程。
The finite element model of fan rotor system parameterization is designed. Modularity programming is developed based on general business finite element analyzing software ALGOR.
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