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Letter from thePresident and CEO,Vi
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Information TechnologyMilton AdamsE
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BiographyMilton Adams has been at D
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Figure 1 represents a functional de
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Programs. In effect, these controll
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Although the terminal area traffic
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Table 2. ATFM performance evaluatio
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In the experiments, a nominal capac
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[3] Wambsganss, Michael C. “Colla
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Guidance, Navigation, and Control A
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A Control Lyapunov FunctionApproach
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x( 0) ∈ X and w(t) ∈Wfor all t
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(b) Select a quadratic RCLF V i (x)
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at each grid point. In the case w 1
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References[1] Ball, J.A. and A.J. v
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Guidance, Navigation, and Control A
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Relative and Differential GPSData T
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The first term on the right in the
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H R# δρ R,GPS -H A# δρ A,GPSThi
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selection; and (3) shown that the a
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Guidance, Navigation, and Control A
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Segmentation of MR ImagesUsing Curv
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(3)where ν now represents a contin
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Experimental ResultsThe results of
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Table 1. A summary of segmentation
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Guidance, Navigation,and ControlJim
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BiographyGeorge SchmidtGeorge Schmi
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clock and ephemeris errors, as well
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maintained in a rigid structure, wh
- Page 61 and 62: Table 5. “Typical” absolute GPS
- Page 63 and 64: performed, then the target location
- Page 65 and 66: tightly-coupled system, however, ca
- Page 67 and 68: Concluding RemarksRecent progress i
- Page 69 and 70: As real-time systems evolve into th
- Page 71 and 72: Advanced Fault-TolerantComputing fo
- Page 73 and 74: The Viking and Voyager were both in
- Page 75 and 76: Containment Regions (FCRs). There a
- Page 77 and 78: well as reversing the whole process
- Page 79 and 80: As real-time systems evolve into th
- Page 81 and 82: Automated Station-Keepingfor Satell
- Page 83 and 84: Figure 2. Minimum elevation angles
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- Page 87 and 88: However, since optimization and rec
- Page 89 and 90: is maintained in the Northern Hemis
- Page 91 and 92: autonomy. It must have the ability
- Page 93 and 94: [31] Neelon, Joseph G., Jr., Paul J
- Page 95 and 96: Draper’s primary goal is to Drape
- Page 97 and 98: )Rotordynamic Modelingof an Activel
- Page 99 and 100: Eq. (9) becomes:λ[ R ] { Φ } = [
- Page 101 and 102: chosen to be 24, for a total of 48
- Page 103 and 104: InertialInstruments/MechanicalDesig
- Page 105 and 106: BiographyJeffrey Borenstein is curr
- Page 107 and 108: process step. Process information i
- Page 109 and 110: Figure 4. Control chart for boron d
- Page 111: References[1] Barbour, N., J. Conne
- Page 115 and 116: Validating the Validating Tool:Defi
- Page 117 and 118: calculates miscellaneous terms, suc
- Page 119 and 120: Table 1. Suggested specification sh
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- Page 125 and 126: Table 2. Sample high-level summary
- Page 127 and 128: AcknowledgmentR.L. Greenspan, J.A.
- Page 129 and 130: Systems IntegrationRich MartoranaPe
- Page 131 and 132: BiographyAnthony Kourepenis is an A
- Page 133 and 134: control is employed to maintain the
- Page 135 and 136: Table 1. Summary of automotive yaw
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- Page 139 and 140: References[1] Greiff, P., B. Boxenh
- Page 141 and 142: Guidance, Navigation, and Control A
- Page 143 and 144: An Integrated Safety AnalysisMethod
- Page 145 and 146: Infrastructure ModelsSystemRequirem
- Page 147 and 148: Figures 6 and 7 illustrate the bloc
- Page 149 and 150: Notice that each flight track descr
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- Page 161 and 162: The 1997 Charles StarkDraper PrizeT
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The 1997 Charles StarkDraper Prize1
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“Draper encourages its personnel
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Gimballed Vibrating GyroscopeHaving
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“Draper encourages its personnel
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Optical Source Isolator withPolariz
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“Draper encourages its personnel
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Hunting Suppressor forPolyphase Ele
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“Draper encourages its personnel
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Sensor Having an Off-Frequency Driv
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proof mass from transients and enha
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1997 Published PapersThe following
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monitoring of space structures and
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measured by kinematic degrees of fr
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i.e., what percent of the earth’s
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McConley, M. W.; Dahleh, M. A.; Fer
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unaffordable, or even misguided. Bu
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The Draper DistinguishedPerformance
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Educational Activitiesat Draper Lab