The following pages link to (Q4979386):
Displaying 4 items.
- Optimal rotation of the orbit plane of a variable mass spacecraft in the central gravitational field by means of orthogonal thrust (Q2289036) (← links)
- 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) (← 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)
- The new algorithm of quasi-optimal reorientation of a spacecraft (Q6488025) (← links)
