Decoupled Direct State Transition Matrix Calculation with Runge-Kutta Methods
Author:
Funder
Air Force Research Laboratory
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Link
http://link.springer.com/article/10.1007/s40295-018-0131-2/fulltext.html
Reference60 articles.
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2. Aristoff, J.M., Horwood, J.T., Poore, A.B.: Orbit and uncertainty propagation: a comparison of Gauss-Legendre-, Dormand-Prince-, and Chebyshev-Picard-based approaches. Celest. Mech. Dyn. Astron. 118(1), 13–28 (2014). https://doi.org/10.1007/s10569-013-9522-7
3. Aristoff, J.M., Poore, A.B.: Implicit Runge-Kutta methods for orbit propagation. In: AAS/AIAA Astrodynamics Specialist Conference, Minneapolis (2012)
4. Aristoff, J.M., Horwood, J.T., Singh, N., Poore, A.B.: Nonlinear uncertainty propagation in orbital elements and transformation to Cartesian space without loss of realism. In: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference, San Diego (2014)
5. Aristoff, J.M., Horwood, J.T., Poore, A.B.: Implicit-Runge-Kutta-based methods for fast, precise, and scalable uncertainty propagation. Celest. Mech. Dyn. Astron. 122(2), 169–182 (2015). https://doi.org/10.1007/s10569-015-9614-7
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