The attitude controller, velocity controller and position controller are designed by the EMPC algorithms.3) Study on the robust stabilityHelicopters are usually disturbed during flight, so the robust stability of the flight controller is very important.
论文采用EMPC算法完成了姿态控制器、速度控制器和位置控制器的设计。 3)鲁棒稳定性研究直升机在飞行中常会受到各种干扰的影响,因此控制器的鲁棒性就成为衡量控制器优良的重要指标。
参考来源 - 基于预测控制的小型无人直升机自主飞行研究Second, on the base of value function of the reinforcement learning algorithm, the attitude controller is designed by tabular method and Gaussian Softmax Basis Function (GSBF) neural network method.
其次,在值函数增强学习算法基础上,利用表格型增强学习算法和GSBF神经网络算法设计姿态控制器。
参考来源 - 基于增强学习的小型无人直升机控制方法研究·2,447,543篇论文数据，部分数据来源于NoteExpress
The system consists of a guidance law and a basic attitude controller.
系统分为基本姿态控制器设计和制导系统设计两个部分进行研究。
The proposed method is applied to satellite attitude controller design to cope with the errors arising while linearization procedure.
将所得结果应用于卫星姿态控制系统的设计，以解决对模型进行线性化处理时产生的误差。
This method is applied to an unmanned helicopter, and the design of an adaptive attitude controller and a trajectory-tracking controller are presented.
本文把该方法应用于无人直升机，给出了自适应姿态控制系统和跟踪控制器的设计方法。
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