An Intelligent Attitude Control Method for UAV Based on DDPG Algorithm

Y.X. Xian, Peng Wang, Hongbo Xin, Yujie Wang, Qing-yang Chen, Z. Hou
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Abstract

The unmanned aerial vehicle (UAV) requires the control system with fast response speed, high accuracy and strong robustness. Due to the strong coupling and nonlinearity of UAV system, it is difficult to build the accurate system model, which makes it difficult for traditional linear control methods to achieve accurate and stable control effects. This paper proposes an intelligent attitude control method for high-speed UAV. Firstly, the nonlinear attitude motion model of UAV is established and a new intelligent attitude controller structure is built based on the Deep Deterministic Policy Gradient (DDPG) algorithm. Secondly, the DDPG attitude controller is trained by the simulation training system. The control simulation results show that the proposed intelligent control system and controller can meet the requirements of attitude adjustment and attitude stabilization, the control accuracy error is less than 0.02 degree. Finally, considering fixed mutation interference, Gaussian noise and 50% deviation of aerodynamic parameters disturbance, the control accuracy error is still less than 0.1 degree during the interference test. The stability analysis shows that the intelligent controller has strong robustness and generalization ability.
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基于DDPG算法的无人机智能姿态控制方法
无人机对控制系统的要求是响应速度快、精度高、鲁棒性强。由于无人机系统的强耦合和非线性,难以建立精确的系统模型,这使得传统的线性控制方法难以达到精确稳定的控制效果。提出了一种高速无人机智能姿态控制方法。首先,建立了无人机的非线性姿态运动模型,并基于深度确定性策略梯度(DDPG)算法构建了一种新的智能姿态控制器结构;其次,利用仿真训练系统对DDPG姿态控制器进行训练。控制仿真结果表明,所提出的智能控制系统和控制器能够满足姿态调整和姿态稳定的要求,控制精度误差小于0.02度。最后,考虑固定突变干扰、高斯噪声和50%偏差的气动参数干扰,干扰试验时控制精度误差仍小于0.1度。稳定性分析表明,该智能控制器具有较强的鲁棒性和泛化能力。
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