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The following pages link to Quaternion methods and regular models of celestial mechanics and space flight mechanics: the use of Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. I: Review and analysis of methods and models and their applications (Q2695821):
Displaying 2 items.
- Quaternion methods and models of regular celestial mechanics and astrodynamics (Q2167671) (← links)
- Quaternion methods and regular models of celestial and space flight mechanic: using Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. II: Perturbed spatial restricted three-body problem (Q2699160) (← links)