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Moving towards a UAV flight with a dynamic inversion controller and a navigation filter

机译:通过动态反转控制器和导航滤波器向UAV飞行移动

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The Kalman Filter is a common method in navigation applications used to fuse data from the Inertial Measuring Unit with the GPS data to estimate a precise position. Dynamic inversion has proven to be a suitable way of controlling nonlinear systems. Both methods result in complex algorithms with a high count of computation cycles. These algorithms are developed in Matlab/Simulink and usually laboriously implemented onto the hardware. In this work autocode techniques are used to program these algorithms directly from Simulink. The aspect of the implementation in relation to the operating system and the computing power are considered.
机译:Kalman滤波器是导航应用中的常用方法,用于熔化来自惯性测量单元的数据与GPS数据来估计精确位置。 动态反演已被证明是控制非线性系统的合适方式。 这两种方法都会导致具有高计数计算周期的复杂算法。 这些算法在Matlab / Simulink中开发,通常在硬件上进行费用。 在此工作中,自动码技术用于直接从Simulink编程这些算法。 考虑了关于操作系统和计算能力的实现的方面。

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