4.3 Article

Real-time optimal techniques for unmanned air vehicles fuel saving

出版社

SAGE PUBLICATIONS LTD
DOI: 10.1177/0954410011418881

关键词

dynamic soaring; trajectory optimization; flight guidance; flight control; estimation

资金

  1. BAe Systems Operations Ltd
  2. EPSRC under the FLAVIIR Programme [GR/S71552/01]
  3. Engineering and Physical Sciences Research Council [GR/S71552/01] Funding Source: researchfish

向作者/读者索取更多资源

Dynamic soaring can save fuel by the extraction of low-altitude wind shear energy. The problem of generating energy-saving trajectories in real time for an unmanned powered sailplane is considered. A method called 'inverse dynamics in the virtual domain' is investigated. The method results in rapid solution generation and is suitable for real-time applications. Three-dimensional unmanned aerial vehicle equations of motion and a non-linear wind gradient-model are used. Trajectories are generated to minimize the total power used per horizontal distance travelled for cross-wind travelling and in the total power used per total time in air for loitering mode. Trajectory following issues are addressed and an architecture for the control system is briefly described. A method for the estimation of wind shear gradient parameters is proposed. Validation is performed using a full six-degree-of-freedom model of a powered sailplane to verify the trajectory generation method.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.3
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据