CIFERÂ®-MATLAB Interfaces: Development and ... - Cal Poly

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© Copyright 2005 Brian K. Rupnik All Rights Reserved ii
Approval Page TITLE: AUTHOR: CIFER ® -MATLAB Interfaces: Development and Application Brian K. Rupnik DATE SUBMITTED: April 2005 Dr. Daniel J. Biezad (AERO) ____________________________________ Advisor & Committee Chair Dr. Mark B. Tischler (NASA/Army) ____________________________________ Committee Member Dr. Eric Mehiel (AERO) ____________________________________ Committee Member Dr. Lanny V. Griffin (CENG) ____________________________________ Committee Member iii
Page 1: CIFER ® -MATLAB Interfaces: Develo
Page 5 and 6: Acknowledgements The author would l
Page 7 and 8: 4.4 ANALYSIS ON SHADOW 200 TUAV....
Page 9 and 10: Figure 4.21: Comparisons with Exact
Page 11 and 12: Chapter 1: Introduction The focus o
Page 13 and 14: 1.1.1 What CIFER ® Encompasses CIF
Page 15 and 16: Figure 1.3: Doublet Example (UAV Fl
Page 17 and 18: One almost universal concern with t
Page 19 and 20: involving handling qualities analys
Page 21 and 22: One key feature of frequency respon
Page 23 and 24: and high-frequency content is captu
Page 25 and 26: Thus the low-frequency content of l
Page 27 and 28: consistency by reconstructing respo
Page 29 and 30: Chapter 3: Programming and Code Dev
Page 31 and 32: interpret it, how to condition it,
Page 33 and 34: Figure 3.1: Name-value Pairs and St
Page 35 and 36: Figure 3.2: Percent Error Compariso
Page 37 and 38: command-line-based interface that r
Page 39 and 40: 3.2.1 Development Process The most
Page 41 and 42: The third screen is used to match w
Page 43 and 44: Chapter 4: Validation and Applicati
Page 45 and 46: Figure 4.2: SISO Mass-Spring-Damper
Page 47 and 48: 4.3 UH-60 Simulation The first in-d
Page 49 and 50: The differences between the two cal
Page 51 and 52: Table 4.3: Cutoff Frequency Results
Page 53 and 54:
Two sets of data were used: one was
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Figure 4.14: Roll Angle to Rate Com
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The same checks were run on the fli
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Figure 4.20: Vertical Velocity Pert
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Figure 4.22: Aileron - Roll Rate Re
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CIFER ® offers a utility for analy
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La Length: Lm = [4.14] N τ a Time
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UAV might conceivably achieve bandw
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FRESPID and MISOSA have been create
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Bibliography Works Cited: 1.) Hamel
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Appendix A: Screen Layout Compariso
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New GUI Interface: Figure A6: MATLA
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Figure A10: MATLAB GUI: Final Scree
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CIFER ® main programs The three ma
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out_f = frespid('XVLATSWP',1); >> o
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The variables that support screen 8
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as input and up to five outputs to
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All the information is displayed to
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to either the linearized phase and
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CIFER ® support utilities: Three f
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Appendix C: Online Help for Main Pr
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id.maxfft SCREEN 9 id.plotopt id.pl
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[out] = composite('TEST',2,'casenam
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misosa Structure fields are: casena
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Function: cifhq Description: This f
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the results will be displayed in th
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in.source SCREEN 2 in.pminfrq in.pm
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cifarith Structure fields are: name
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and magnitude must be included. Oth
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c_in.outputs(1) c_in.frcalc(1,1) c_
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% Set up blank composite case c_in
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CIFERÂ®-MATLAB Interfaces: Development and ... - Cal Poly

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