Publication Date:
2019-06-28
Description:
NASA Langley Research Center has, for several years, conducted research in the area of time-correlated gust loads for linear and nonlinear aircraft. The results of this work led NASA to recommend that the Matched-Filter-Based One-Dimensional Search Method be used for gust load analyses of nonlinear aircraft. This manual describes this method, describes a FORTRAN code which performs this method, and presents example calculations for a sample nonlinear aircraft model. The name of the code is MFD1DS (Matched-Filter-Based One-Dimensional Search). The program source code, the example aircraft equations of motion, a sample input file, and a sample program output are all listed in the appendices.
Keywords:
AIRCRAFT STABILITY AND CONTROL
Type:
NASA-TM-109768
,
NAS 1.15:109768
,
AD-A278236
,
DOT/FAA/CT-93/63
Format:
application/pdf
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