推力矢量飞机平衡特性研究

通过建立推力矢量飞机数学模型，分析其平衡状态的基本特征，利用连续算法对其平衡面进行计算，以及对其仿真结果比较分析，介绍推力矢量技术的发展状况，从而全面理解推力矢量系统配置下飞机的优越机动性能。

Research on the Equilibrium Characteristic of Thrust Vectored Aircraft

This paper introduces the developing status of TVC and advantage of thrust vectoring system with establishing the math model of thrust vectored aircraft, analyzing the characteristic of equilibrium states in steady flight of an aircraft, and using continuation methods to calculate equilibrium surface and comparing with the simulation result.