Abstract
This paper describes the development of an approximate method for propagating uncertainty through stochastic dynamical systems using a quadrature rule integration based method. The development of quadrature rules for Gaussian mixture distributions is discussed. A numerical solution to this problem is considered that uses a Gram-Schmidt process. The new approach is applied to the attitude estimation problem. The proposed method outperforms the unscented Kalman filter for attitude estimation for scenario with large initial error.
Original language | English (US) |
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Pages (from-to) | 3735-3753 |
Number of pages | 19 |
Journal | Advances in the Astronautical Sciences |
Volume | 148 |
State | Published - 2013 |
Event | 23rd AAS/AIAA Space Flight Mechanics Meeting, Spaceflight Mechanics 2013 - Kauai, HI, United States Duration: Feb 10 2013 → Feb 14 2013 |