What is it about?
Regularized orbit propagation theory with lunar perturbation to overcome physical and computational difficulties due to singularities.
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Why is it important?
We found very low errors when compared with other integrators. It can be used in mission software development, in onboard applications for faster computation and easy to implement.
Perspectives
Can be useful for future space industry with cube and nano-sats.
Harishkumar Sellamuthu
Karunya University
Read the Original
This page is a summary of: Orbit Theory with Lunar Perturbation in Terms of Kustaanheimo–Stiefel Regular Elements, Journal of Guidance Control and Dynamics, November 2016, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g002342.
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