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

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3. Nelson, R.C. Flight Stability and Automatic Control, 2 nd ed., New York: McGraw-Hill, Inc., 1998. 4. Nise, N.S., Control Systems Engineering, New York: John Wiley & Sons, Inc., 2000. 5. Nyhoff, L.R., Leestma, S.C., Fortran 90 for Engineers and Scientists, New Jersey: Prentice Hall, 1997. 6. Thurling, A.J., “Improving UAV Handling Qualities Using Time Delay Compensation,” M.S. Thesis, Air Force Institute of Technology, 2000. 7. Tischler, M.B., Cauffman, M.G., "Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO-105 Coupled Rotor/Fuselage Dynamics," Journal of the American Helicopter Society, Vol 37, No 3, pgs 3-17, July 1992. 62
Appendix A: Screen Layout Comparison This Appendix contains a series of screen shots that show each screen in COMPOSITE for both the original CIFER ® screen interface and the new GUI interface. A more detailed description of the differences can be found in Chapter 3. Old Interface: Figure A1: Original Interface: Screen 1 Figure A2: Original Interface: Screen 2 63
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CIFER ® -MATLAB Interfaces: Develo
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Approval Page TITLE: AUTHOR: CIFER
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Acknowledgements The author would l
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4.4 ANALYSIS ON SHADOW 200 TUAV....
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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
Page 55 and 56: Figure 4.14: Roll Angle to Rate Com
Page 57 and 58: The same checks were run on the fli
Page 59 and 60: Figure 4.20: Vertical Velocity Pert
Page 61 and 62: Figure 4.22: Aileron - Roll Rate Re
Page 63 and 64: CIFER ® offers a utility for analy
Page 65 and 66: La Length: Lm = [4.14] N τ a Time
Page 67 and 68: UAV might conceivably achieve bandw
Page 69 and 70: FRESPID and MISOSA have been create
Page 71: Bibliography Works Cited: 1.) Hamel
Page 75 and 76: New GUI Interface: Figure A6: MATLA
Page 77 and 78: Figure A10: MATLAB GUI: Final Scree
Page 79 and 80: CIFER ® main programs The three ma
Page 81 and 82: out_f = frespid('XVLATSWP',1); >> o
Page 83 and 84: The variables that support screen 8
Page 85 and 86: as input and up to five outputs to
Page 87 and 88: All the information is displayed to
Page 89 and 90: to either the linearized phase and
Page 91 and 92: CIFER ® support utilities: Three f
Page 93 and 94: Appendix C: Online Help for Main Pr
Page 95 and 96: id.maxfft SCREEN 9 id.plotopt id.pl
Page 97 and 98: [out] = composite('TEST',2,'casenam
Page 99 and 100: misosa Structure fields are: casena
Page 101 and 102: Function: cifhq Description: This f
Page 103 and 104: the results will be displayed in th
Page 105 and 106: in.source SCREEN 2 in.pminfrq in.pm
Page 107 and 108: cifarith Structure fields are: name
Page 109 and 110: and magnitude must be included. Oth
Page 111 and 112: c_in.outputs(1) c_in.frcalc(1,1) c_
Page 113: % Set up blank composite case c_in
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CIFERÂ®-MATLAB Interfaces: Development and ... - Cal Poly

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