This article researches on mathematical model of the control mechanism of the thrust-vectoring nozzle. Some reasonable simplification methods are used to build this model because the control mechanism is very complication.
本文通过对矢量喷管控制机构运动规律的深入分析，采用合理的简化方法，对一些隐函数关系进行了显示化处理，建立了矢量喷管控制机构的运动学数学模型，该模型在计算精度和实时性上满足了控制要求。
参考来源 - 矢量喷管控制机构运动学模型建模及其与发动机综合控制研究·2,447,543篇论文数据，部分数据来源于NoteExpress
The mathematical model of turbofan engine transient process with thrust vectoring nozzle was established.
建立带矢量喷管的涡扇发动机动态数学模型。
As thrust vectoring nozzle is the feature of advanced fighters, the difficulties in implementing thrust vectoring are summarized.
矢量喷管是先进战斗机的特征，本文讨论了实现推力矢量存在的技术难点。
Internal performance of unsteady flow of counterflow thrust vectoring nozzle has researched base on numerical simulation.
基于数值模拟方法，研究了逆流矢量喷管非定常内流性能。
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