摘要
To eliminate the drawback that INS (inertial navigation system) errors are accumulated with time, a tightly-coupled INS/SMNS (Scene Matching Navigation System) integrated navigation system is put forward for unmanned aerial vehicles (UAV). It can roughly position the UAV and correct the geometric distortion of real-time graph by INS-provided position and orientation information. Therefore, the real-time and precision in suitable-matching area of SMNS can be improved obviously. Meanwhile, the accumulation error of INS is corrected by using the high-accuracy positioning of SMNS. With the complementary advantages between SMNS and INS, the tightly-coupled INS/SMNS navigation system can obtain significantly improved real-time performance and accuracy. The experiment results show that the proposed system meets the route planning requirements of UAV.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 302-306 |
| 页数 | 5 |
| 期刊 | Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology |
| 卷 | 18 |
| 期 | 3 |
| 出版状态 | 已出版 - 6月 2010 |
指纹
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