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Spacecraft Attitude Determination and Control J.R. Wertz
Publisher: Springer

The GRADe study has investigated attitude determination areas offering potential applicability to spacecraft attitude determination. WERTZMicrocosm Inc., Torrance, CA . Examples include telemetry, telecommand and data acquisition (i.e. Spacecraft Attitude Determination & Control. Such systems, once It is becoming clear that these micro and nano systems can replace all the subsystems of satellites including central computers, communications, power, propulsion, attitude control and inertia measurement units, as well as payload instruments. IIIf IIIIIIII I I I I I I I I I SPACECRAFT ATTITUDE DETERMINATION AND CONTROLEdited byJAMES R. The ACS uses the spacecraft computer to perform closed loop attitude determination and control. Payload - accomplishes mission specific tasks and varies greatly between missions. SRP, as described above, is among the potential propellantless-propulsion approaches. A spacecraft system comprises various subsystems, dependent upon mission profile. Especially effects of delay and disturbance), ground station design and implementation, formation flying, and attitude determination. Extensive work has been done for many years in the areas of attitude determination, attitude prediction, and attitude control. V0=magnetometer bias =the net local magnetic intensity in body coordinates. [2] Wertz, J.R., Spacecraft Attitude Determination and Control, Dordrecht,.