Gravity gradient measurementsIt is shown that, for floated satellite gradiometers subject to very low levels of unmodeled forces and torques, dynamic estimation can dramatically reduce rotation correction errors. The filter structure is developed, and the value of factorization techniques is examined. Numerical examples are given for a few practical cases using plausible instrument ensembles. To achieve these early results, great simplifications have been made, and important error sources have been suppressed.
Document ID
19890041200
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sonnabend, D. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mceneaney, W. M. (California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)