Title: Flight instrumentation specification for parameter identification: Program user's guide
Abstract: A set of four digital computer programs is presented which can be used to investigate the effects of instrumentation errors on the accuracy of aircraft and helicopter stability-and-control derivatives identified from flight test data. The programs assume that the differential equations of motion are linear and consist of small perturbations about a quasi-steady flight condition. It is also assumed that a Newton-Raphson optimization technique is used for identifying the estimates of the parameters. Flow charts and printouts are included.
Publication Year: 1975
Publication Date: 1975-06-01
Language: en
Type: article
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