Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Method and apparatus for using a momentum bias to provide spacecraft attitude stabilization during an eclipse

Method and apparatus for using a momentum bias to provide spacecraft attitude stabilization during an eclipse

US Patent 6260806 · Granted Jul 17, 2001

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Relocatable field programmable gate array bitstreams for fault tolerance2011
Compact window heating unit utilizing pelletized fuel2010
Ash handling and treatment in solid fuel burners2010
Grate structure for solid fuel burners2007
Method of operating a satellite for end-of-life maneuvers2006
Refractory wall structure and damper device2005
Method of operating a satellite for end-of-life maneuvers2004
Safing mode for high momentum states in body stabilized spacecraft2003
Method and apparatus for operating satellites in orbit2002
Stationkeeping method utilizing open-loop thruster pulses and closed-loop author2002
Free return lunar flyby transfer method for geosynchronous satellites havint mul2000
Free return lunar flyby transfer method for geosynchronous satellites2000