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Joint state and parameter estimation of quadrotor based on extended Kalman filter and complementary filter

机译:基于扩展卡尔曼滤波和互补滤波的四旋翼联合状态和参数估计

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In this paper the problem of joint state and parameter estimation of quadrotor is addressed. It was assumed that quadrotor is equipped with Inertial Measurement Unit (IMU) and GPS module. Based on this instrumentation it was possible to estimate complete state vector describing the movement of rigid body, along with parameters related to its propulsion system and aerodynamic properties. Author original solution based on use of extended Kalman filter and complementary filter is presented. Performance of proposed algorithm is evaluated by means of numerical simulation.
机译:本文解决了四旋翼的关节状态和参数估计问题。假定四旋翼飞机装有惯性测量单元(IMU)和GPS模块。基于这种仪器,可以估计描述刚体运动的完整状态矢量,以及与推进系统和空气动力学特性相关的参数。提出了基于扩展卡尔曼滤波器和互补滤波器的作者原始解决方案。通过数值仿真对所提出算法的性能进行了评估。

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