Pivot actuated nutation damping system for a dual-spin...

Details Pivot actuated nutation damping system for a dual-spin... Pivot actuated nutation damping system for a dual-spin...

G - Physics

05

D

244/1.2

G05D 1/10 (2006.01) B64G 1/28 (2006.01) B64G 1/38 (2006.01) G05D 1/08 (2006.01) B64G 1/26 (2006.01)

Patent

CA 1282393

PIVOT ACTUATED NUTATION DAMPING SYSTEM FOR A DUAL-SPIN SPACECRAFT Abstract of the Disclosure A nutation damping system for a dual-spin satellite is provided by tilting the rotation axis of the spacecraft's spinning body in one direction away from the normal spin axis of the satellite, and a half nutation period later tilting the axis in the opposite direction back to the normal axis. The one direction of tilting is toward the angular momentum vector component that is transverse to the spinning body's spin axis.

521915

Affiliated with

Also associated with

Rating

Pivot actuated nutation damping system for a dual-spin... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Pivot actuated nutation damping system for a dual-spin..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Pivot actuated nutation damping system for a dual-spin... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1340250