Sensor-fault tolerant attitude determination using two-stage estimator

Author:

Byeon SooYung,Mok Sung-Hoon,Woo Hyunwook,Bang Hyochoong

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference23 articles.

1. Real-time sensor fault detection and isolation for LEO satellite attitude estimation through magnetometer data;Adnane;Adv. Space Res.,2018

2. Byeon, S.Y., Koh, D.W., Woo, H.W., Sayegh, A.M.A., 2017. Performance analysis of spacecraft maneuver to calibrate attitude determination subsystem. In:AAS/AIAA Space Flight Mechanics Meeting, San Antonio, TX, USA, February 5–9.

3. Cheon, Y.-J., 2005. Unscented filtering in a unit quaternion space for spacecraft attitude estimation. In: International Conference on Control, Automation, and Systems 2005.

4. Fault detection and isolation of satellite inertial instrumentation using nonlinear adaptive filter;Das;J. Aerospace Inform. Syst.,2015

5. Survey and future directions of fault-tolerant distributed computing on board spacecraft;Fayyaz;Adv. Space Res.,2016

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