A report describes a method of detecting leakage in one of the 16 thrusters of the Cassini spacecraft. The detection method, implemented as part of the spacecraft flight software, is based on the fact that the three-axis rotational motion of a spacecraft is governed by the Euler's equation. The left-hand side of the Euler's equation contains both the inertia and gyroscopic torques, which are estimated by the attitude estimator of the attitude control software. The right-hand side of the Euler's equation contains reaction torques from both the thrusters and the reaction wheels which are also estimated.

This work was done by Allan Y. Lee of NASA's Jet Propulsion Laboratory. To obtain a copy of the report, "A Model-based Thruster Leakage Monitor for the Cassini Spacecraft" access the Technical Support Package (TSP) free on-line at www.techbriefs.com under the Mechanics category. NPO-20441

NASA Tech Briefs Magazine

This article first appeared in the April, 1999 issue of NASA Tech Briefs Magazine.

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