2006-2007 - Kennedy Space Center Technology Transfer Office

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Bird Vision SystemThe Bird Vision system is a multicamera photogrammerty software application thatSpaceport/RangeSituational runs on a Microsoft Windows XP platform and was developed at Kennedy SpaceAwareness Center by ASRC Aerospace. This software system collects data about the locations ofbirds within a volume centered on the Space Shuttle and transmits it in real time to thelaptop computer of a test director in the Launch Control Center (LCC) Firing Room. The qualitycontrolledbird location data is also transmitted to the Firing Room bird tracking console, startingat the end of the T–9-minute hold. This data is available until T–60 seconds, when the trackeroperators take control of the cameras and the Bird Vision application is terminated. This systemuses the pad tracking cameras at three camera sites located about 1,200 feet from the pad, near theinside of the pad perimeter. The Bird Vision system backs up the Bird Radar system and includes thefollowing features:• 3-D Model Plot Mode (both local and remote overlay displays) provides real-time rotation,zoom, and translation of the 3-D view, using the mouse controls against a 3-D CAD modelbackground and terrain map. There are several views for this display, including top view, sideview, perspective view, and flyby view (rotating perspective view), which can be set via the 3-DModel Settings Tab.• 3-D Overlay Plot Mode (both local and remote overlay displays) provides real-time rotation,zoom, and translation of the 3-D view, using the mouse controls.• Triangulation (both local and remote overlay displays): For every pair of cameras set toBroadcast Mode, a circle is plotted on the 2-D overlay if the intersecting camera view linespass within a maximum distance threshold, thus indicating a high probability of a bird at thatlocation in 3-D space. The user may select the maximum distance threshold (the default is2.5 m). A solid sphere is plotted in the 3-D Plot Mode where two camera view lines pass withinthis maximum distance threshold.• The Bird Track (local overlay display only) generates a pseudo bird track by plotting a historyof triangulated positions and then applying a fading-color function to the plot symbol. Thisfeature is enabled when the number of history plots equals a nonzero value under the BirdVision system control panel. The default value is 1.• The system has the ability to record all processed data (camera view lines as well as triangulatedpositions) sent to the LCC Bird Vision remote display. This feature allows the test director toreview all bird tracking data immediately following a launch or a scrub.Vision system calibration is accomplished by markingthe top and bottom positions of the pad lightning maststructure.Manually drawing exclusive regions of interest helps mitigatefalse detections from background noise.60 Range Technologies
Plot Overlay Mode, where a yellow circle represents the 3-D intersection of all pairs of twocameraview lines to a detected object (bird).3-D Model Plot Mode.Contact: Dr. John E. Lane , ASRC Aerospace, (321) 867-6939Participating Organizations: NASA-KSC (Dr. Robert C. Youngquist, Charles G. Stevenson, andStephen J. Payne) and ASRC Aerospace (Dr. Christopher D. Immer, Jesus A. Dominguez, and Herbert W. Oleen)KSC Technology Development and Application 2006-200761
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ForewordSuccessful technology devel
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ContentsSpaceport Structures and Ma
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Contents (continued)Process and Hum
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IntroductionJohn F. Kennedy Space C
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Constellation SystemsSurfaceSystems
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Spaceport Structures and MaterialsK
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20181614∆ E1210Modified Sensor Be
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Initial results of the EDEM model o
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Contacts: Dr. Carlos I. Calle ,NASA
Page 23 and 24: Close examination of the corrosions
Page 25 and 26: Adhesion at Failure (psi)2500200015
Page 27 and 28: Figure 1. After 500 hours of salt f
Page 29 and 30: Contacts: Dr. Paul E. Hintze , NASA
Page 31 and 32: Figure 2. Repairs to various types
Page 33 and 34: on top of the cuvette contains the
Page 35 and 36: Figure 2. A corrugated NiTi sheet e
Page 37 and 38: The PLTD can be used to (1) calibra
Page 39 and 40: SEM images of neat MWNT fibers: (a)
Page 41 and 42: Contacts: Trent M. Smith
Page 43 and 44: Figure 1. An isometric cutaway view
Page 45 and 46: Figure 2. Quartz sand flowing in th
Page 47 and 48: Figure 2. Top images show how the e
Page 49 and 50: Sand volume fraction contour at t =
Page 51 and 52: Integrated LWRD/RVC engineering bre
Page 53 and 54: Mean relative percentage change in
Page 55 and 56: We compared the model’s predictio
Page 57 and 58: Figure 2. Three-dimensional simulat
Page 59 and 60: Figure 3. Camera calibration model.
Page 61 and 62: The sketch in Figure 2 shows alaunc
Page 63: Figure 2. Signal generator (right)
Page 66 and 67: Hail Size Distribution MappingA 3-D
Page 68 and 69: Launch Pad 39 Hail Monitor Array Sy
Page 70 and 71: Autonomous Flight Safety System - P
Page 72 and 73: The Photogrammetry CubeSpaceport/Ra
Page 76 and 77: Automating Range Surveillance Throu
Page 78 and 79: Next-Generation Telemetry Workstati
Page 80 and 81: GPS Metric Tracking UnitAs Global P
Page 82 and 83: Space-Based RangeSpace-Based Range
Page 85 and 86: Fluid System TechnologiesKSC Techno
Page 87 and 88: 0.900.850.80Discharge Coefficient,
Page 89 and 90: Composite seals for performance eva
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Page 93 and 94: Contacts: Dr. Barry J. Meneghelli ,
Page 95 and 96: 60555045Comparative k-value (mW/m-K
Page 97 and 98: a compatible spacecraft model where
Page 99 and 100: In an ongoing effort for improvemen
Page 101: Low-gravity probe prototype test.th
Page 104 and 105: Countermeasure for Radiation Protec
Page 106 and 107: Focused Metabolite Profiling for Di
Page 109 and 110: Process and Human FactorsEngineerin
Page 111 and 112: DON uses game technology to enable
Page 113 and 114: Type of mobile crane that impacted
Page 115 and 116: SALT proof-of-concept communication
Page 117 and 118: SSLM CAD model.Our design offers th
Page 119 and 120: Variables that can be integrated by
Page 121: Exploration Supply Chain Simulation
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Nanosensors for Evaluating Hazardou
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Sixty-four-Channel Inline Cable Tes
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Wireless Inclinometer Calibration S
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Generating Safety-Critical PLC Code
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Spacecraft Electrostatic Radiation
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Ion Beam Propulsion StudySpacecraft
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RT-MATRIX: Measuring Total Organic
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Appendix AKSC High-Priority Technol
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Risk Assessment ToolMission Data Fe
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Appendix BInnovative Partnership Pr
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system for the Government, using th
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tracking objects after launch, and
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2006-2007 - Kennedy Space Center Technology Transfer Office

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