Pages that link to "Item:Q2699160"
From MaRDI portal
The following pages link to 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):
Displaying 2 items.
- Quaternion methods and models of regular celestial mechanics and astrodynamics (Q2167671) (← links)
- Quaternion methods and regular models of celestial mechanics and space flight mechanics: local regularization of the singularities of the equations of the perturbed spatial restricted three-body problem generated by gravitational forces (Q6180784) (← links)