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Research on relative navigation algorithm for UAV Autonomous Aerial Refueling rendezvous phase

机译:无人机自主空中加油交会阶段的相对导航算法研究

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The lack of Autonomous Aerial Refueling capability is one of the greatest limitations of UAV (unmanned aerial vehicle). The estimation of the relative position, velocity and attitude is the key issue in this research area. This paper proposes a novel method for relative navigation. We focus on the need for the rendezvous phase. The structure of this paper is as follows. Firstly, we shall briefly introduce the autonomous aerial refueling phases and the related navigation sensors. Then we establish the error equation. After using the Kalman filter, we obtain the estimation of the relative state error. The employed algorithm based on the SINS/GPS/IRST integrated relative navigation, it has advantages of both autonomous navigation and passive target positioning. In simulation experiments, the results show that our algorithm can track the relative state variation and restrain the error divergency effectively.
机译:缺乏自主空中加油能力是无人机(无人机)的最大局限之一。相对位置,速度和姿态的估计是该研究领域中的关键问题。本文提出了一种相对导航的新方法。我们专注于会合阶段的需求。本文的结构如下。首先,我们将简要介绍自主空中加油阶段以及相关的导航传感器。然后我们建立误差方程。使用卡尔曼滤波器后,我们获得相对状态误差的估计。所采用的基于SINS / GPS / IRST的组合相对导航算法,具有自主导航和被动目标定位的优点。在仿真实验中,结果表明我们的算法可以跟踪相对状态变化并有效地抑制误差发散。

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