• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文期刊>Transactions of the Japan society for aeronautical and space sciences >Turning Direction Determination using Error Dynamics-Based Guidance Law for Stationary Target Observation
【24h】

Turning Direction Determination using Error Dynamics-Based Guidance Law for Stationary Target Observation

机译：基于误差动力学的制导律确定静止目标的转弯方向

获取原文
获取原文并翻译 | 示例
           
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

Guidance laws are proposed to enable unmanned aerial vehicles (UAVs) to accomplish stationary target observation missions. In this paper, a nonlinear guidance law is designed utilizing the characteristics of distance error dynamics. The turning direction of the UAVs is very important for multiple UAVs operation. The turning direction of UAV is related to the line-of-sight angular acceleration of the UAV. The proposed guidance law is analyzed to provide a guideline for selecting guidance gains taking into consideration the turning direction. Numerical simulations are performed to verify the performance of the proposed guidance law.
机译：提出了制导法，以使无人飞行器（UAV）能够完成固定的目标观察任务。本文利用距离误差动态特性设计了非线性制导律。无人机的转向对于多个无人机的运行非常重要。无人机的转向与无人机的视线角加速度有关。对拟议的制导律进行了分析，以提供考虑转向方向的选择制导增益的指导。进行数值模拟以验证所提出的制导律的性能。

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