NASA NTRS · 19810014193
INDES User's guide multistep input design with nonlinear rotorcraft modeling
Abstract
The INDES computer program, a multistep input design program used as part of a data processing technique for rotorcraft systems identification, is described. Flight test inputs base on INDES improve the accuracy of parameter estimates. The input design algorithm, program input, and program output are presented.
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1979-11-01. INDES User's guide multistep input design with nonlinear rotorcraft modeling. https://ntrs.nasa.gov/citations/19810014193
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