Trajectory Planning using Nonlinear Receding Horizon Optimization for an Autonomous Airship

Sohan Suvarna, Hoam Chung, A. Sinha, R. Pant
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Abstract

This paper presents a control architecture for reference tracking of a small autonomous airship with input constraints. Nonlinear receding horizon optimization is used in order to generate a reference trajectory for the low-level controller to track. A simplified lateral dynamics model for an airship is also presented in this paper to be used for prediction. To investigate the efficacy of the proposed control algorithm, it is then implemented on a simulation platform and tested on a 6-degrees-of-freedom airship model to track a straight line and circular trajectory in the presence of wind disturbance. The simulation results indicate that the proposed planner generates a feasible trajectory for the low-level controller to track. A significant improvement in the tracking performance of the airship is also seen by the introduction of the planner.
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基于非线性后退地平线优化的自主飞艇轨迹规划
提出了一种具有输入约束的小型自主飞艇参考跟踪控制体系结构。为了生成参考轨迹供底层控制器跟踪,采用了非线性后退水平优化。本文还提出了一个简化的飞艇横向动力学模型,用于预测。为了验证所提出的控制算法的有效性,在一个仿真平台上实现了该算法,并在一个6自由度飞艇模型上进行了风干扰下直线和圆形轨迹的跟踪测试。仿真结果表明,该规划器生成了可行的轨迹供低层控制器跟踪。飞艇跟踪性能的显著改进也被规划器的引入所看到。
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