期刊文献+

面向空地协同的旋翼无人机动平台自主降落最优轨迹生成

Optimal Trajectory Generation for Autonomous Landing of Rotorcraft on a Moving Platform for Air-ground Coordination
原文传递
导出
摘要 旋翼无人机在移动平台上快速自主降落能够提升空地机器人的任务适应性和作业灵活性,对提高任务响应速度和增强救援能力具有重要意义。为了使旋翼无人机在最短时间内安全降落到移动平台,本文提出了一种最优升力分解轨迹生成方法,旨在在升力有限的情况下,最大化旋翼无人机的飞行性能。该方法首先对旋翼无人机的有限升力进行分解,获得最优的3轴升力分配,然后将非线性加速度约束转化为动态线性约束,最后根据最优控制理论求解出最优飞行时间轨迹。仿真结果表明了本文提出的算法能够保证轨迹生成的准确性和稳定性,并且该算法的计算效率高,能够满足系统实际应用中的实时性要求。 The fast autonomous landing of rotorcraft on a moving platform can improve the adaptability and flexibility of air-ground robots,which is important for improving mission response speed and enhancing rescue capabilities.In order to achieve the rotorcraft landing on the moving platform in the shortest time,this paper proposes a trajectory generation method for optimal lift decomposition,aiming to maximize the flight performance of the rotorcraft with finite lift.The method decomposes the finite lift of the rotorcraft to obtain the optimal three-axis lift distribution,then transforms the nonlinear acceleration constraint into a dynamic linear constraint,and finally solves the optimal time-of-flight trajectory of the rotorcraft according to the optimal control theory.The simulation results show that the proposed algorithm can ensure the accuracy and stability of trajectory planning,and the algorithm has high computational efficiency,which can meet the real-time requirements of the system in practical applications.
作者 郑勇杰 张广玉 杨丽英 黄朝雄 ZHENG Yongjie;ZHANG Guangyu;YANG Liying;HUANG Zhaoxiong(State Key Laboratory of Robotics,Shenyang Institute of Automation,Chinese Academy of Sciences,Shenyang 110016,China;Institutes for Robotics and Intelligent Manufacturing,Chinese Academy of Sciences,Shenyang 110169,China;University of Chinese Academy of Sciences,Beijing 100049,China)
出处 《机器人》 EI CSCD 北大核心 2024年第3期266-274,283,共10页 Robot
基金 国家自然科学基金(U22B2041,61991413,91948303)。
关键词 旋翼无人机 空地协同 轨迹生成 升力分解 动平台降落 rotorcraft air-ground coordination trajectory generation lift decomposition landing on moving platform
  • 相关文献

参考文献1

二级参考文献5

共引文献22

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部