An Autonomous Navigation Algorithm Using Geomagnetic Sensor and Star Sensor

Cai Min Chen; Bao Hua Li; Chang Hong Wang; Rui Liu

doi:10.4028/www.scientific.net/AMR.650.449

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 650An Autonomous Navigation Algorithm Using...

An Autonomous Navigation Algorithm Using Geomagnetic Sensor and Star Sensor

Abstract:

Aiming at the limitations of the orbital dynamic equations based star sensor navigation method, a star sensor /geomagnetic information utilized aircraft autonomous navigation method is proposed. Dynamic equations applicable to general aircrafts are established. System observation equations are deduced. The angle between geomagnetic and starlight vector is used as observation in the algorithm. Extended Kalman filter is used to estimate position and velocity of aircraft in the algorithm. Singular value decomposition method is used to analyze observability of the system. Simulation results show that the algorithm has many advantages including high precision, good filtering convergence and stability, and non-accumulated error. The algorithm can be used as aided navigation of inertial navigation or in occasions, which only require a general navigation precision.

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Periodical:

Advanced Materials Research (Volume 650)

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449-454

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.650.449

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Online since:

January 2013

Authors:

Cai Min Chen, Bao Hua Li, Chang Hong Wang, Rui Liu

Keywords:

Autonomous Navigation, Geomagnetic Sensor, Star Sensor

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