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 |
|---|---|
| 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 |
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