INS/SMNS tightly-coupled navigation for unmanned aerial vehicle

Yao Jun Li, Quan Pan, Chun Hui Zhao, Ying Yu, Jun Wei Li

Research output: Contribution to journalArticlepeer-review

3 Scopus citations

Abstract

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.

Original languageEnglish
Pages (from-to)302-306
Number of pages5
JournalZhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology
Volume18
Issue number3
StatePublished - Jun 2010

Keywords

  • INS
  • Integrated mode
  • Scene matching navigation system
  • Tightly-coupled
  • Unmanned aerial vehicle

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