Aircraft and Rotorcraft System Identification: Engineering Methods with Flight-Test Examples

Appendix A: Summary of Suggested Guidelines

Table A.1: Suggested guidelines

Guideline

Topic

Chap.

Page

Eq.

? f ? 5 ? max

Select the filter cutoff frequency ? f, also referred to as the filter bandwidth, to be at least five times the maximum frequency of interest of model applicability ? max

5

89

5.1

? s ? 5 ? f

Choose a sample rate ? s, the same for all of the signals, with a value of at least a factor of 5 above the filter frequency ? f

5

90

5.2

T rec ? (4 to 5) T max

For frequency sweeps, the minimum total record length T rec relative to the length of the longest period T max in a record

5

93

5.11

Lower limit of the coherence function to achieve acceptable accuracy in a frequency-response identification (In addition, the coherence function should not be oscillating.)

7

166

7.54

n d ? 5

Minimum number of independent time-history averages n d in a concatenated record

7

169

7.57

T win = 2 T max

Nominal window size T win relative to the length of the longest period of interest T max

7

170

7.60

T win ? 0.5 T rec

Maximum window size T win relative to the length of the record T rec

7

171

7.61

T win ? (1/5) T F

Maximum window size T win relative to the concatenated record length T F

7

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