2012 Second International Conference on Business Computing and Global Informatization 2012
DOI: 10.1109/bcgin.2012.159
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Tightly Coupled GPS/INS Integrated Navigation Algorithm Based on Kalman Filter

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“…It overcomes the defects that the output information errors of the SINS accumulate over time and the measurements of BDS are easily affected by the environment. Therefore, SINS/BDS has been widely used in the design of aircraft navigation systems [2][3][4]. However, with the development of hypersonic vehicles, the rapid increase of flight speed makes the flight environment of the aircraft change rapidly in a short time; it will cause the aircraft to be disturbed by more uncertain factors.…”
Section: Introductionmentioning
confidence: 99%
“…It overcomes the defects that the output information errors of the SINS accumulate over time and the measurements of BDS are easily affected by the environment. Therefore, SINS/BDS has been widely used in the design of aircraft navigation systems [2][3][4]. However, with the development of hypersonic vehicles, the rapid increase of flight speed makes the flight environment of the aircraft change rapidly in a short time; it will cause the aircraft to be disturbed by more uncertain factors.…”
Section: Introductionmentioning
confidence: 99%