首页> 外文会议>International Conference on Space Information Technology; 20071115-17; Wuhan(CN) >Spacecraft's Automatic Landing Control based on online tracing identification method of neural network
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Spacecraft's Automatic Landing Control based on online tracing identification method of neural network

机译:基于神经网络在线跟踪识别方法的航天器自动着陆控制

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To improve the dynamical property and decoupling capability for a class of spacecraft system with strong coupling, a neuron-network controller based on online tracing identification is established to meet the decoupling requirements of multivariable system. The model with new structure and learning algorithm has significance for weight matrices and makes training process of weights become more distinct and straightforward. The new neural network is then applied to identification of nonlinear dynamics system, which the speed of learning and convergence is improved greatly for using the priori input-output state knowledge. The results of simulation show that the neuron network decoupling controller based on online tracing identification can effectively reduce the identification errors caused by the different sampling data, and improve prominently the precision and the reliability of neural network in the system identification. The controller has powerful self-learning and self-adaptive decouple capabilities.
机译:为了提高一类强耦合航天器系统的动力学特性和解耦能力,建立了基于在线跟踪识别的神经网络控制器,以满足多变量系统的解耦需求。具有新结构和学习算法的模型对权重矩阵具有重要意义,使权重的训练过程更加清晰直接。然后将新的神经网络应用于非线性动力学系统的辨识,利用先验输入输出状态知识极大地提高了学习和收敛速度。仿真结果表明,基于在线跟踪辨识的神经元网络解耦控制器可以有效地减少由于采样数据不同而引起的辨识误差,显着提高神经网络在系统辨识中的精度和可靠性。该控制器具有强大的自学习和自适应解耦功能。

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