thrust vector control system

Study on model reference robust control of thrust vector control system

推力矢量控制系统的参考模型鲁棒控制研究

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Model reference fuzzy control ( MRFC) is introduced for a classical thrust vector electrohydraulic servo control system.

针对典型的推力矢量电液位置伺服系统提出参考模型模糊控制控制方法（MRFC）。

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The effects of the extendible exit cone on stability of the thrust vector control system of largescale solid rocket motor are presented and the measures for improving the system stability are suggested.

介绍了喷管可延伸出口锥对大型固体火箭发动机推力向量控制系统稳定性的影响，并提出了改善其系统稳定性的措施。

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This method increase the damping ratio of the thrust vector control system and improve the system performance.

该方法提高了推力矢量电液位置伺服系统阻尼比，改善了系统的动态性能。

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The Effects of the Extendible Exit Cone on Stability of the Thrust Vector Control System

可延伸出口锥对推力向量控制系统稳定性的影响

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Dynamic calculation on thrust vector control system for solid rocket motor

固体火箭发动机推力向量控制系统动力学计算

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Nozzle is an important part of the thrust vector control system of solid rocket motor and high-performance design of a nozzle plays an important role in the performance of the motor.

喷管是固体火箭发动机推力向量控制系统的重要组成部分，高效能的喷管设计对发动机的性能至关重要。

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The program and calculation for thrust vector control system

推力向量控制方案及计算

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On the other hand, close loop model fuzzy control is studied for a classical thrust vector electrohydraulic servo control system with low damping ratio and improves dynamic performance of the system.

此外，本文根据电液位置伺服系统阻尼比低的特点，采用闭环模型模糊控制，改善了系统的动态性能。

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In this paper, model reference robust control ( MRRC) is introduced for a classical thrust vector electrohydraulic servo control system with parameter disturbance and additive uncertainty, which makes it possible for the system to be insensitive to the disturbance and uncertainty.

本文针对典型的推力矢量电液位置伺服系统中存在的参数摄动和加性扰动，采用模型参考鲁棒控制方法（MRRC），使系统对扰动不敏感。

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A methodology based upon the H ∞ principle of weighting sensitivity function loop-shaping is given to design the robust controller of flight control system for vector thrust nozzle.

采用加权灵敏度函数环路成形的H∞准则，给出了矢量推力喷管飞行控制系统的一种鲁棒控制器设计方法。

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Unsteady characteristic research of startup process of secondary hot gas injection thrust vector control system

燃气二次喷射推力矢量控制系统启动过程非定常效应研究

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