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EOS Integrated Payload Articulation and Identification
An Approach to Autonomous Attitude Control for Spacecraft
Twenty Milliarcsec Pointing System for the Rolling GPB
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AACS acceleration accuracy actuator Adv v66 algorithm angle angular antenna arc second array assembly Astronautics attitude control attitude control system attitude determination axes axis bandwidth boresight burn CMG momentum command component configuration control law control loop deadband delta psi detector developed DGCMG disturbance dither double-gimbal dynamic electronics error estimate EXOSAT Figure filter flight frequency function gimbal gyro gyro drift hardware inertial initial input integration launch limit cycle magnitude maneuver manipulator measurements mission mode module momentum management momentum storage motion noise operation optical output parameters payload performance perigee phase pitch platform pointing position pseudorange reaction wheels rotation satellite sensor sequence SGCMG shown in Fig signal simulation single-gimbal CMG slew slew rate solar Space Station spacecraft stability starlocking structure subsystem system identification techniques telemetry telerobot telescope thruster TOPEX torque tracking vector vehicle velocity