A BLENDED FEEDBACK VARIABLE FOR CONTROL AUGMENTATION SYSTEMS.
Technical rept. May 66-Apr 67,
GENERAL ELECTRIC CO BINGHAMTON N Y AVIONIC CONTROLS DEPT
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A man-airframe disturbance sensitivity model has been postulated. The existence of optimum pilot chosen compensation in the multiloop compensatory mode is shown to result in minimum closed loop sensitivity to pilot induced stick input errors. Based on existing fixed base simulator data it is shown that an optimum ratio exists for blended feedback control of pitch rate and normal acceleration. Author
- Human Factors Engineering and Man Machine Systems