Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Optimal sun safe attitude for satellite ground tracking

Optimal sun safe attitude for satellite ground tracking

US Patent 7823836 · Granted Nov 2, 2010

Estimated economic value: $11,554,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Systems and methods for satellite orbit and momentum control2020
Combined orbit and attitude determination system and methods2018
Efficient stationkeeping design for mixed fuel systems in response to a failure 2018
Efficient stationkeeping design for mixed fuel systems2017
Approach for control redistribution of coriolis vibratory gyroscope (CVG) for pe2017
High bandwidth Coriolis vibratory gyroscope (CVG) with in-situ bias self-calibra2017
Methods and apparatus for controlling a plurality of satellites using node-synch2016
Combined location and attitude determination system and methods2015
Enhanced compound steering law for general low thrust mission2015
Compound steering law for efficient low thrust transfer orbit trajectory2013
System and methods for simultaneous momentum dumping and orbit control2013
Simultaneous momentum dumping and orbit control2012