What is it about?
computing exact terms of higher order state transition tensors for perturbed (200x200) orbital motion using computational differentiation.
Featured Image
Read the Original
This page is a summary of: Exact Computation of High-Order State Transition Tensors for Perturbed Orbital Motion, Journal of Guidance Control and Dynamics, March 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g003897.
You can read the full text:
Contributors
The following have contributed to this page
