Extended Kalman filter synthesis for integrated global positioning/inertial navigation systems

@article{Faruqi2000ExtendedKF,
  title={Extended Kalman filter synthesis for integrated global positioning/inertial navigation systems},
  author={Farhan A. Faruqi and Kenneth J. Turner},
  journal={Applied Mathematics and Computation},
  year={2000},
  volume={115},
  pages={213-227}
}
The integrated global position system (GPS)/inertial navigation system (INS) is a cost-e€ective way of providing an accurate and reliable navigation system for civil and military aviation. These systems also provide low cost solutions to mid-course navigation and guidance of mediumand long-range weapon systems. In this paper, an error model developed earlier is used for GPS/INS ®lter mechanization (F.A. Faruqi, Derivation of an integrated GPS/INS non-linear ®lter model, QUT Report: AEAV/FAF… CONTINUE READING
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