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基于SINS/GPS组合导航的无人机安控策略仿真验证 被引量:1

Simulation and Verification of the UAV'S Control Strategy Based on SINS /GPS Integrated Navigation
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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。 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.
作者 蒋志华 陈曦
机构地区 中国人民解放军
出处 《宇航计测技术》 CSCD 2014年第4期37-40,共4页 Journal of Astronautic Metrology and Measurement
关键词 安控策略 组合导航 无人机 Control strategy Integrated navigation UAV
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