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
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 design of the flight controller that exploits the advantages of the nonlinear dynamic inversion, adaptive fuzzy system and slide model control is discussed.
论述了综合运用非线性动态逆、自适应模糊系统和滑模控制的优点进行飞行控制律设计的方法。
The base control law is designed in nonlinear dynamic inversion, and neural networks are used to cancel the inversion error induced by many reasons, especially by actuator failures.
飞机的基本控制律采用非线性动态逆方法设计，对于模型不准确和舵面故障等因素导致的逆误差采用神经网络进行在线补偿。
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