A Study of a Reconnaissance Surveillance Vehicle

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Targeting Accuracy Targeting Timeliness Image Quality Flexibility (User friendly) Utility Model Utility Elements MILITARY UTILITY • Best system selection • Cost effective balance Others # <strong>of</strong> UAV’s Required for Continuous <strong>Surveillance</strong> Area Coverage per Day # Targets per Day Survivability NPS041003 82
Design Implementation & Design Specifics NPS041003 83
Page 1 and 2:
A Study of a Reconnaissance Surveil
Page 3 and 4:
GENERAL UAV ISSUES NPS041003 3
Page 5 and 6:
STRATEGIC • Worldwide OPS • Sel
Page 7 and 8:
Risk Reduction • Never attempt to
Page 9 and 10:
Design to Cost Lowest costs are ach
Page 11 and 12:
Redundancy • Level of Redundancy
Page 13 and 14:
DMS (Diminishing Mfg Sources) - Obs
Page 15 and 16:
Learn from Others’ Mistakes NPS04
Page 17 and 18:
Design Requirements NPS041003 17
Page 19 and 20:
50,000 Ft Steady 20Kt Crosswind Com
Page 21 and 22:
System Selection NPS041003 21
Page 23 and 24:
Continuous coverage Analysis Approa
Page 25 and 26:
Original Design Objective Balance M
Page 27 and 28:
The HALE vehicle - (High Altitude L
Page 29 and 30:
Configuration Development NPS041003
Page 31 and 32: Loral Systems, San Jose, CA Tier II
Page 33 and 34: System Overview Wide-band data tran
Page 35 and 36: Carbon wing, tail and engine nacell
Page 37 and 38: Design Performance NPS041003 37
Page 39 and 40: Wing Lift Coefficient 1.40 1.20 1.0
Page 41 and 42: Design Implementation & Design Spec
Page 43 and 44: Navigation & Guidance Schematic NPS
Page 45 and 46: Maintainability / Accessibility Acc
Page 47 and 48: Integrated Sensor Suite NPS041003 4
Page 49 and 50: Daytime IR Imagery: March 26, 1999
Page 51 and 52: Global Hawk Airborne Integrated Com
Page 53 and 54: Air Vehicle-to-Ground Stations Inte
Page 55 and 56: All-Encompassing System Development
Page 57 and 58: . Pre-flight Checkout Remove before
Page 59 and 60: Mission Start WPt • INS alignment
Page 61 and 62: Temperature ~ Degrees F 100 60 20 -
Page 63 and 64: VN Diagram Global Hawk Vn Diagram L
Page 65 and 66: Gust Exceedance (1000 Hrs) Gust Exc
Page 67 and 68: An Example of a Flight Control HCI
Page 69 and 70: The Air Vehicle Status HCI H367-024
Page 71 and 72: Examples of Autonomous Operations N
Page 73 and 74: Post-flight Checks NPS041003 73
Page 75 and 76: Summary 1. UAVs will demonstrate lo
Page 77 and 78: Typical Dual VMS Aircraft Loss Rate
Page 79 and 80: Design Requirements NPS041003 79
Page 81: Affordability UFP COTS Interchangea
Page 85 and 86: Electrical Power Schematic NPS04100
Page 87 and 88: Vehicle Fuel System Schematic NPS04
Page 89 and 90: Single Event Upsets >≅ 40 K Ft Co
Page 91 and 92: AV2 -4 T urb ulence Even t.5 Altitu
Page 93 and 94: Turbulence Event Conclusions � Fl
Page 95 and 96: Typical Fault Logic, Lost Carrier N
Page 97 and 98: Airspace Coordination Requirements
Page 99: Civil Surveillance Requirements NPS
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A Study of a Reconnaissance Surveillance Vehicle

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