US Patent No: 5,935,176

Number of patents in Portfolio can not be more than 2000

Momentum wheel oscillation filter

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Abstract

Momentum wheel speed correction in an orbital space vehicle that corrects for the oscillation resulting from spurious variations in the angular velocity of the momentum wheel. The momentum wheel's angular velocity is subject to random fluctuations due to Coulomb forces. These fluctuations are coupled into the vehicle's spin rate causing errors in the yaw rate and yaw. By adding corrective values to the determined yaw rate and yaw by selectively filtering the momentum wheel tachometer signals, pointing errors are substantially reduced or even eliminated.

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First Claim

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Patent Owner(s)

Patent OwnerAddressTotal Patents
LOCKHEED MARTIN CORPORATIONBETHESDA, MD5429

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Nielson, Marlin C Boulder, CO 3 24

Cited Art

Patent Info (Count) # Cites Year
 
LOCKHEED MARTIN CORPORATION (7)
5,020,745 Reaction wheel fricton compensation using dither 30 1989
5,058,835 Wheel speed management control system for spacecraft 31 1990
5,343,398 Spacecraft roll-yaw compensator with orbit-rate and harmonic bandpass filters 10 1992
5,248,118 Spacecraft attitude control system with reaction wheel bearing protection 18 1992
5,608,634 Low noise spacecraft body rate sensing arrangement for attitude control 15 1992
5,308,024 Disturbance torque compensated three axis yaw control system 30 1992
5,610,820 Minimum propellant, zero momentum spacecraft attitude control system 19 1995
 
AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE (2)
5,259,577 Attitude control system for three-axis stabilized satellite in near-equatorial orbit 20 1991
5,269,483 Continuously acting one-way satellite roll-yaw attitude control method and device 15 1992
 
HUGHES ELECTRONICS CORPORATION (2)
5,184,790 Two-axis attitude correction for orbit inclination 20 1991
5,540,405 Method and apparatus for compensating for magnetic disturbance torques on a satellite 11 1993
 
SPACE SYSTEMS/LORAL, INC. (2)
4,521,855 Electronic on-orbit roll/yaw satellite control 35 1981
4,931,942 Transition control system for spacecraft attitude control 21 1988
 
INTELSAT SERVICES CORPORATION (1)
4,911,385 Attitude pointing error correction system and method for geosynchronous satellites 26 1987
 
MATRA (1)
4,294,420 Attitude control systems for space vehicles 26 1978
 
MATRA MARCONI SPACE UK LIMITED (1)
4,786,018 Satellite attitude control 8 1987
 
MESSERSCHMITT-BOLKOW-BLOHM GMBH (1)
4,567,564 Arrangement for the attitude stabilization of flexible vehicles with weakly-dampened structural vibrations and discontinuous control intervention 23 1981
 
RCA CORPORATION (1)
4,230,294 Closed loop roll control for momentum biased satellites 30 1979

Patent Citation Ranking

Forward Cites

Patent Info (Count) # Cites Year
 
NSK STEERING SYSTEMS CO., LTD. (1)
7,382,105 Motor driving device and electric power steering apparatus 1 2004
 
THE BOEING COMPANY (1)
6,860,451 Spacecraft spin axis reorientation method 2 2003