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| | Pre-bias scheme for roll momentum unloads on pitch momentum bias/yaw reaction wheel spacecraft - US Patent 6439509 (Site not responding. Last check: 2007-10-09) |
 | | In dealing with short-term transients due to disturbances such as roll momentum unloads, currently the spacecraft is biased in roll angle, approximately 50% of the magnitude, in the opposite direction of the expected transient. |
 | | Each system involves orientation sensing components and means for adjusting the orientation of the craft including magnetic torquers, momentum wheels, and thrusters, which alter and unload unwanted momentum resulting from imposed forces from solar torque, thruster firing, fuel shift, and such. |
 | | The present invention is directed to such a system for controlling and reducing short-term transients caused by disturbances, such as roll momentum unloads, and utilizes the spacecraft nutation damper, particularly the nutation compensator, in achieving this end. |
| www.patentstorm.us /patents/6439509.html (1606 words) |
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