首页> 外文期刊>Mathematical Problems in Engineering >UAV Formation Flight Based on Nonlinear Model Predictive Control
【24h】

UAV Formation Flight Based on Nonlinear Model Predictive Control

机译:基于非线性模型预测控制的无人机编队飞行

获取原文
获取原文并翻译 | 示例
           

摘要

We designed a distributed collision-free formation flight control law in the framework of nonlinear model predictive control. Formation configuration is determined in the virtual reference point coordinate system. Obstacle avoidance is guaranteed by cost penalty, and intervehicle collision avoidance is guaranteed by cost penalty combined with a new priority strategy.
机译:我们在非线性模型预测控制的框架内设计了一种分布式无碰撞编队飞行控制律。地层配置在虚拟参考点坐标系中确定。成本惩罚可确保避免障碍,而成本惩罚与新的优先级策略相结合可确保避免车辆碰撞。

著录项

  • 来源
    《Mathematical Problems in Engineering》 |2012年第2期|p.643-657|共15页
  • 作者单位

    Department of Control Engineering, Naval Aeronautical and Astronautical University,YanTai 264001, China;

    Department of Control Engineering, Naval Aeronautical and Astronautical University,YanTai 264001, China;

    Department of Control Engineering, Naval Aeronautical and Astronautical University,YanTai 264001, China;

    Department of Control Engineering, Naval Aeronautical and Astronautical University,YanTai 264001, China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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