Variable periodic disturbance rejection filter

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

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701 4, 701 10, 701226, 244164, 244169, B64G 128, G06F16500

Patent

active

059447613

ABSTRACT:
A filter for use in an attitude control system which may be subjected to vibrations from disturbances which have frequency contents that vary with time. Sensors on the system produce signals that contain the disturbance frequencies and a calculator connected to the source of disturbance produces a signal which varies as a function of the disturbance. The filter receives these signals and augments the control loop gain at the disturbance frequencies thereby enabling the attitude control devices to null the disturbance effects on the attitude of the system.

REFERENCES:
patent: 5459669 (1995-10-01), Adsit et al.
patent: 5765780 (1998-06-01), Barskey et al.

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