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NASA NTRS · 19740007265

Multi-input, multi-output regulator design for constant disturbances and non-zero set points with application to automatic landing in a crosswind

Abstract

Undesirable steady offsets result when a stationary, linear regulator using state feedback is subjected to constant disturbances and/or non-zero setspoints. To eliminate these offsets, the disturbances and non-zero setpoints can be fed forward to the control. Only when the number of outputs is less than or equal to the number of control inputs can the outputs be maintained at arbitrary non-zero setpoints. The state and the disturbance may be estimated using a constant gain Kalman filter or by modeling the constant disturbances as exponentially correlated processes with long correlation times.

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BibTeXRIS

Holley, W. E., Bryson, A. E., Jr.. 1973-08-01. Multi-input, multi-output regulator design for constant disturbances and non-zero set points with application to automatic landing in a crosswind. https://ntrs.nasa.gov/citations/19740007265

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