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Comprehensive System Identification
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APROVAL PAGETITLE:AUTHOR:Comprehens
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ACKNOWLEDGMENTSThe author would lik
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3.4.4 Magnetometer Identification..
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LIST OF FIGURESFigure 1.1 - Land Wa
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Figure 3.48 - Magnetometer Depictio
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CHAPTER 1 - INTRODUCTION AND MOTIVA
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The vehicles examined within the sc
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tunnel testing to study the charact
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Figure 1.8 - Helicopter Body Axes S
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GPSRate GyrosAccelerometersIMUInner
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CHAPTER 2 - METHODS AND TECHNIQUES2
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2.2.1 Flight Test TechniquesThere a
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manufacturer specifications are mod
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3.2 Bare-Airframe IDThe bare-airfra
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Table 3.2 - OAV Frequency Range of
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⎧ p⎫⎪ ⎪y = ⎨q⎬⎪ r ⎪
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Table 3.4 - OAV DERIVID Identified
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The identified state-space model yi
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Better sensors, at higher sampling
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Figure 3.3 - Yaw response frequency
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Figure 3.4 shows that even though t
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It can be seen that the Aerovironme
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3.2.2 Allied Aerospace MAVFlight te
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30MAGNITUDE(DB)-10-50250PHASE(DEG)5
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A 0th/2nd order transfer function i
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Figure 3.12 shows the same for the
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Techsburg) the pitching moment resp
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Table 3.11 shows that all of the di
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Figure 3.14 shows how increasing th
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the duct, the effects of the man ne
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ft-lbMu PLATFORM= 5.11ftsecThis dim
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apparent that the size of the duct
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adequate way to characterize the di
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actuators varied in size, weight, c
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It is noticeable from the figure th
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Table 3.17 - Actuator Calibration F
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Figure 2.1 shows an example frequen
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The test matrix is provided as Tabl
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frequency response curves shown in
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Table 3.22 shows that for the first
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The time delays all seemed to be ar
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400035003000250020001500y = -13429x
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higher data rates, and tighter tole
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esponse and the response obtained f
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The time histories show that the ou
- Page 93 and 94: Figure 3.31 - Magnitude Comparison
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- Page 109 and 110: Figure 3.43 shows that gyros were m
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- Page 113 and 114: Figure 3.46 shows the modeled fluct
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- Page 117 and 118: Figure 4.1 - Simulink MAV ModelFigu
- Page 119 and 120: Figure 4.3 - Simulink Sweep Generat
- Page 121 and 122: cause a pitching moment to be exert
- Page 123 and 124: Figure 4.6 - Cross Control Decoupli
- Page 125 and 126: ⎡ Lp Lq Lr Lu Lv Lw0 0 0⎤⎢MpM
- Page 127 and 128: It can be seen right away that the
- Page 129 and 130: Figure 4.8 shows that the coherence
- Page 131 and 132: CHAPTER 5 - CONCLUSIONSThe need for
- Page 133 and 134: 6. Mettler, B., Tischler, M. B., an
- Page 135 and 136: Appendix AOAV Proposal VehicleIdent
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- Page 139 and 140: HS512MG - 5V- 127 -
- Page 141 and 142: DS368 - 5V- 129 -
- Page 143: 94091 - 5V- 131 -
- Page 147 and 148: Appendix CActuator Generated Transf
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- Page 151 and 152: DS8417 - 100% - 6V- 139 -
- Page 153 and 154: HS512MG - 100% - 5V- 141 -
- Page 155 and 156: HS512MG - 100% - 6V- 143 -
- Page 157 and 158: DS368 - 100% - 5V- 145 -
- Page 159 and 160: DS368 - 100% - 6V- 147 -
- Page 161 and 162: 94091 - 80% - 5V- 149 -
- Page 163 and 164: 94091 - 80% - 6V- 151 -
- Page 165 and 166: CS-10BB - 100% - 5V- 153 -
- Page 167 and 168: CS-10BB - 100% - 6V- 155 -
- Page 169 and 170: Appendix DActuator Time Domain Veri
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- Page 173 and 174: DS368 5VDS368 6V- 161 -