而原本曾经因为此类意外事件发生机率过低、被认为不合乎经济效益而被搁置的推力控制飞机（Propulsion-Controlled Aircraft，PCA）之开发研究也再度受到重视，配备有这种技术的飞机能够在完全不靠液压控制飞航介面的情况下，利用电脑精密地...
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但调查人员发现，这起事故有可能是一个严重的非对称推力（具体指两台发动机推力不同）问题造成了左滚，导致飞机失去控制。
The investigators found that the circumstances of this accident indicate that a severe asymmetric thrust condition caused a left roll that led to loss of control of the airplane.
采用QFT理论设计了某型飞机的纵向着陆控制律，并应用了推力综合控制稳定飞机下滑时的速度。
In this paper a longitudinal robust automatic landing control law was designed by QFT approach combine with thrust controls.
常规线性飞控系统针对推力矢量飞机这样的多控制冗余、非线性MIMO系统，无法实现非线性控制。
Conventional linear flight control systems do not satisfy nonlinear control requirement of aircraft with thrust vector, which is a multiple control redundances and nonlinear MIMO system.
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