论文信息 - ESTIMATION OF SPACECRAFT MASS PROPERTIES USING ANGULAR RATE GYRO DATA

ESTIMATION OF SPACECRAFT MASS PROPERTIES USING ANGULAR RATE GYRO DATA

On-orbit estimation of spacecraft mass properties can be useful for planning of maneuvers and potentially for determination of spacecraft fuel load. In this paper we describe the application of a weighted-least-squares parameter estimation technique to simulated and onorbit gyro data for the purpose of determining spacecraft mass properties.

Bruce V. Burlton | John Palimaka

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