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E. A. R. Anstey


Click on the titles below to find US government-authored or -collected reports written by E. A. R. Anstey

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Real Time Operational Control of Miranda. FEB 1976
Authors:  E. A. R. Anstey; M. J. Hammond; ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (ENGLAND)
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.This Report describes the automatic control techniques developed and used for the operational control of Miranda (X4), the first British 3-axis stabilised satellite. The operational control techniques are a development of those used for Prospero and the more important improvements are described. Explanation of, and experience in the use of these techniques during the lifetime of the satellite are given. (Author)


Miranda: Operations for Two 'Electronically Disturbed' Passes. FEB 1976
Authors:  M. J. Hammond; E. A. R. Anstey; E. Jones; ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (ENGLAND)
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.The operational activities at the RAE Satellite Control Centre on the mornings of 10 March and 21 May 1974 when the Miranda satellite was in an 'electronically disturbed' state are described. The controller returned the satellite to its planned state using automatic techniques within the timescale of each pass and thus prevented possible mission failure. (Author)


REDUCTION OF ERRORS IN MAGNETIC ASPECT SENSORS BY A SYSTEM OF GROUND CALIBRATION. MAR 1966
Authors:  C. T. Farr; E. A. R. Anstey; ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (ENGLAND)
The full text of this report is not available and therefore is not for sale. This information is provided for reference purposes only.The report discusses the limitations and sources of error introduced into magnetic aspect sensors when installed in a sounding rocket. Typical values of the errors resulting from the magnetic properties of the rocket and its associated electromagnetic instrumentation are given. An attempt to reduce the errors by pre-flight calibration of the rocket head is discussed, and the techniques employed in the method given. Other methods by which the errors may ...


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