首页> 外文会议>Proceedings of the the Institute of Navigation 2007 national technical meeting (ION NTM 2007) >Vision-only Navigation and Control of Unmanned Aerial Vehicles Using the Sigma-Point Kalman Filter
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Vision-only Navigation and Control of Unmanned Aerial Vehicles Using the Sigma-Point Kalman Filter

机译:使用Sigma-Point Kalman滤波器的无人驾驶飞机的仅视觉导航和控制

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This paper presents the vision-only navigation and control of a small autonomous helicopter given only measurements from a video camera fixed on the ground. The goal is to develop an alternative to traditional INS/GPS and on-board vision aided systems. rnThe autonomous navigation and control of the helicopter is achieved using a nonlinear state estimator and a statedependent controller. A key difference to INS/GPS navigation is that measurements of the helicopter’s accelerations and angular velocities are not directly available. The state estimation combines the vision measurements with a dynamic model of the vehicle in a recursive filtering procedure using a Sigma-Point Kalman Filter (SPKF). The estimation of the helicopter’s current state (position, attitude, velocity, and angular velocity) is then fed back in real-time to a state-dependent Riccati equation (SDRE) controller to generate radio control commands to the helicopter. rnSimulations are provided comparing performance relative to INS/GPS navigation. Experiments also show that an accurate dynamic model of the vehicle is necessary for closed-loop stability. Our results indicate the feasibility of designing a vision-only estimation and control system capable of stabilizing and maneuvering a small unmanned helicopter.
机译:本文仅给出了固定在地面上的摄像机的测量结果,给出了小型自主直升机的视觉导航和控制。目标是开发一种替代传统INS / GPS和车载视觉辅助系统的解决方案。 rn直升机的自主导航和控制是使用非线性状态估计器和状态相关的控制器实现的。 INS / GPS导航的主要区别在于无法直接获得直升机加速度和角速度的测量值。状态估计在使用Sigma-Point Kalman滤波器(SPKF)的递归过滤过程中将视觉测量结果与车辆的动态模型结合在一起。然后,将直升机当前状态(位置,姿态,速度和角速度)的估计值实时反馈到与状态有关的Riccati方程(SDRE)控制器,以生成对直升机的无线电控制命令。提供了仿真,比较了与INS / GPS导航相关的性能。实验还表明,车辆的精确动态模型对于闭环稳定性是必要的。我们的结果表明,设计能够稳定和操纵小型无人直升机的仅视觉估计和控制系统的可行性。

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