Pages that link to "Item:Q734022"

The following pages link to The problem of optimal control of the orientation of an orbit of a spacecraft as a deformable figure (Q734022):

Displaying 5 items.

• Optimal reorientation of a Spacecraft's orbit using a jet thrust orthogonal to the orbital plane (Q900318) (← links)
• Design of the suboptimal profiled relay control of orientation of the spacecraft having elastic structural elements with regard for two oscillation tones (Q1778637) (← links)
• Optimal control of the orientation of systems of rigid and deformable bodies in a central field of force (Q1901549) (← 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)
• Optimal Reorientation Of Spacecraft Orbit (Q3453359) (← links)