Nonlinear dynamic inversion control law can better solve the problem of super-maneuver flight control, by which the thesis simulate cobra maneuver and herbst maneuver, and research on system robustness.
非线性动态逆控制律能够较好地解决对战斗机超机动飞行的控制问题。 本文采用该算法对眼镜蛇机动和赫布斯特机动进行了全状态仿真,并研究了系统的鲁棒性。
参考来源 - 攻击机群空战数据链和火力控制的研究与仿真·2,447,543篇论文数据，部分数据来源于NoteExpress
This paper presents a dynamic inversion control method for high Angle - of - attack flight.
提出了一种飞机大仰角飞行的动态逆模糊集成控制方法。
The nonlinear dynamic inversion controller based on online neural net is adopted for the attitude control loop.
基本姿态控制器采用基于在线神经网络的非线性动态逆控制器。
The networks are trained by the fast BP algorithm via fuzzy variables decision, and training samples are provided by the dynamic inversion control results.
网络的训练利用改进的BP算法，将因子模糊化快速进行。样本点数据则由利用动态逆控制所得到的结果来提供。
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