An autonomous celestial navigation method for LEO satellite based on unscented Kalman filter and information fusion
- 30 April 2007
- journal article
- Published by Elsevier BV in Aerospace Science and Technology
- Vol. 11 (2-3), 222-228
- https://doi.org/10.1016/j.ast.2006.12.003
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- SINS/ANS integration for augmented performance navigation solution using unscented Kalman filteringAerospace Science and Technology, 2006
- Space-time registration of radar and ESM using unscented Kalman filterIEEE Transactions on Aerospace and Electronic Systems, 2004
- The unscented Kalman filter for nonlinear estimationPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- Autonomous navigation of high-Earth satellites using celestial objects and Doppler measurementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- Spacecraft orbit determination using GPS navigation solutionsAerospace Science and Technology, 2000
- A new method for the nonlinear transformation of means and covariances in filters and estimatorsIEEE Transactions on Automatic Control, 2000
- Autonomous navigation using the TDRSS Onboard Navigation System (TONS)Advances in Space Research, 1995
- Ground tests of magnetometer-based autonomous navigation (MAGNAV) for low-earth-orbiting spacecraftJournal of Guidance, Control, and Dynamics, 1993
- Autonomous satellite navigation by stellar refractionJournal of Guidance, Control, and Dynamics, 1984