Inflight observability of gyro reference frame misalignment
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Engineering topics
Publications and source records attributed to Huang, Whittak H..
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Error in approximation less than computer truncation error. Report discusses scheme for reduction of computational drift in estimation of attitude of spacecraft from strapdown-gyroscope measurements.
The Magellan low cost interplanetary mission spacecraft, scheduled for flight in 1989, employs a computer-based Attitude and Articulation Control System (AACS) that interfaces with spacecraft sensors and actuators. The sensors include two attitude reference units, a star-scanner unit, two digital sun sensors, and a tachometer. The actuators encompass three reaction wheels, a total of 12 attitude control thrusters, eight attitude-control engines, a solar array drive assembly, and an input-output drive assembly. A detailed account is given of the AACS's onboard computer architecture.