宇航计测技术
• 论文 • 上一篇 下一篇
蒋志华1;陈曦1
出版日期:
发布日期:
作者简介:
JIANG Zhi-hua1;CHEN Xi1
Online:
Published:
摘要: 针对无人机在海上与陆上飞行环境的差异,建立了基于SINS/GPS的组合导航系统数学模型。通过故障模拟,对导航系统在GPS接收机失效工作状态下的性能进行了仿真,并由仿真结果验证了相应安控策略的可行性,无人机可飞至陆上进行伞降回收,具有工程参考价值。
关键词: 安控策略, 组合导航, 无人机
Abstract: Aim at the difference of UAV flying environment between the offshore and onshore, the math model is constructed based on SINS/GPS integrated navigation. The navigation performance is simulated in the condition of GPS failure, the results indicate the control strategy is correct, the UAV can be parachute recovered on land and have a great engineering application value.
Key words: Control strategy, Integrated navigation, UAV
蒋志华;陈曦. 基于SINS/GPS组合导航的无人机安控策略仿真验证[J]. 宇航计测技术, doi: 10.12060/j.issn.1000-7202.2014.04.09.
JIANG Zhi-hua;CHEN Xi. Simulation and Verification of the UAV′S Control Strategy Based on SINS/GPS Integrated Navigation[J]. JOURNAL OF ASTRONAUTIC METROLOGY AND MEASUREMENT, doi: 10.12060/j.issn.1000-7202.2014.04.09.
0 / / 推荐
导出引用管理器 EndNote|Ris|BibTeX
链接本文: http://www.yhjcjs.com.cn/CN/10.12060/j.issn.1000-7202.2014.04.09
http://www.yhjcjs.com.cn/CN/Y2014/V34/I4/37