...
首页> 外文期刊>IFAC PapersOnLine >Planar Inequality Constraints for Stable, Collision-free Model Predictive Control of a Quadcopter
【24h】

Planar Inequality Constraints for Stable, Collision-free Model Predictive Control of a Quadcopter

机译:四轴飞行器稳定,无碰撞模型预测控制的平面不等式约束

获取原文
   

获取外文期刊封面封底 >>

       

摘要

This paper presents a stable, suboptimal, collision-free target tracking technique for a quadcopter based on convex Model Predictive Control. It develops an approximate linear state-space model for the quadcopter dynamics by linearizing around a hover condition. The quadcopter’s path is constrained by a sequence of planes tangent to the surface of obstacles. When implemented in a receding horizon, the orientation of these planes adapt to changes in the environment. A softened terminal constraint is used to improve stability characteristics while avoiding feasibility errors. The sequence of control actions are expressed as perturbations on a stabilizing feedback law expanded over a finite prediction horizon. Simulations demonstrate the technique can be used to avoid spherical obstacles in a target tracking scenario.
机译:本文提出了一种基于凸模型预测控制的四轴飞行器稳定,次优,无碰撞目标跟踪技术。通过围绕悬停条件进行线性化,它为四轴飞行器动力学开发了一个近似的线性状态空间模型。四轴飞行器的路径受到与障碍物表面相切的一系列平面的约束。当在后退的地平线上实施时,这些平面的方向会适应环境的变化。使用软化的终端约束条件可提高稳定性,同时避免可行性误差。控制动作的序列表示为对在有限的预测范围内扩展的稳定反馈定律的摄动。仿真表明,该技术可用于避免目标跟踪场景中的球形障碍。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号