Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle
Patent
1998-03-16
2000-10-03
Louis-Jacques, Jacques H.
Data processing: vehicles, navigation, and relative location
Vehicle control, guidance, operation, or indication
Aeronautical vehicle
701 3, 701 4, 701226, 701222, 244166, 244168, 244169, 244165, G06F 1700, G06G 776
Patent
active
061285560
ABSTRACT:
Control moment gyros in an array are rotated to reorient a satellite. Gyro angle is selected from one of three values based upon whether the stored angular momentum for the desired angle is below a singularity free value, greater than the singularity free value or is greater than the maximum available stored angular momentum.
REFERENCES:
patent: 4746085 (1988-05-01), Bruderle
patent: 4949922 (1990-08-01), Rosen
patent: 5025381 (1991-06-01), Goodzeit et al.
patent: 5608634 (1997-03-01), Goodzeit et al.
patent: 5667171 (1997-09-01), Fowell et al.
patent: 5681012 (1997-10-01), Rosmann et al.
patent: 5765780 (1998-06-01), Barskey et al.
patent: 5806804 (1998-09-01), Goodzeit et al.
Krzysztof Tehori and Robert Muszynski, "Singular Inverse Kinematic Problem For Robotic Manipulators: A Normal Form Approach" (Feb. 1998).
S. R. Vadali and S. Krishnan, "Suboptimal Command Generation For Control Moment Gyroscopes and Feedback Control of Spacecraft" (Nov.-Dec. 1995).
Mark D. Kuhns and Armando A. Rodriguez, "Singularity Avoidance Control Laws for a Multiple CMG Spacecraft Attitude Control System" (Jun. 1994).
Greenstien Robert E.
Honeywell International , Inc.
Louis-Jacques Jacques H.
LandOfFree
CMG control based on angular momentum to control satellite attit does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with CMG control based on angular momentum to control satellite attit, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and CMG control based on angular momentum to control satellite attit will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-204148