Application of Least Mean Square Algorithms to Spacecraft Vibration Compensation

This paper describes the application of the Least Mean Square (LMS) algorithm in tandem with the Filtered-X Least Mean Square algorithm for controlling a science instrument’s line-of-sight pointing. Pointing error is caused by a periodic disturbance and spacecraft vibration. A least mean square algo...

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Veröffentlicht in:The Journal of the astronautical sciences 1998-01, Vol.46 (1), p.83-90
Hauptverfasser: Woodard, Stanley E., Nagchaudhuri, Abhijit
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Nagchaudhuri, Abhijit
description This paper describes the application of the Least Mean Square (LMS) algorithm in tandem with the Filtered-X Least Mean Square algorithm for controlling a science instrument’s line-of-sight pointing. Pointing error is caused by a periodic disturbance and spacecraft vibration. A least mean square algorithm is used on-orbit to produce the transfer function between the instrument’s servo-mechanism and error sensor. The result is a set of adaptive transversal filter weights tuned to the transfer function. The Filtered-X LMS algorithm, which is an extension of the LMS, tunes a set of transversal filter weights to the transfer function between the disturbance source and the servo-mechanism’s actuation signal. The servo-mechanism’s resulting actuation counters the disturbance response and thus maintains accurate science instrumental pointing. A simulation model of the Upper Atmosphere Research Satellite is used to demonstrate the algorithms.
doi_str_mv 10.1007/BF03546194
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subjects Actuation
Actuators
Adaptive filters
Algorithms
Computer simulation
Control equipment
Error analysis
Least squares approximations
Mean square values
Servomechanisms
Spacecraft
Spacecraft vibration
Transfer functions
Transversal filters
Upper atmosphere
Vibration control
title Application of Least Mean Square Algorithms to Spacecraft Vibration Compensation
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