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© 2015 Rockwell Collins. All rights reserved.
Rockwell Collins Proprietary Information© 2015 Rockwell Collins. All rights reserved.
Rockwell Collins Proprietary Information
Combined Vision Systems -HUD, Enhanced Vision and Synthetic Vision Systems
Aviation Electronics Europe Conference Munich March 26, 2015
ENHANCED VISION SYSTEMS
© 2015 Rockwell Collins. All rights reserved.
Rockwell Collins Proprietary Information 2
EFVS Value Proposition
• Enhanced Flight Vision System (EFVS)– EVS image displayed conformal head up
• Lower taxi / landing / takeoff operating minima
– Fewer go arounds
– Lower fuel costs
© 2015 Rockwell Collins. All rights reserved.
Rockwell Collins Proprietary Information
– Lower fuel costs
– Fewer delays/cancellations
– Increased loyalty/revenue
• Seeing in low visibility / darkness
– Fewer runway incursions
– Collision avoidance
3
EFVS Lower Minimums in EuropeEU OPS 1 Amendment 2
• Pilot using EFVS may continue to 100’ if a visual reference is displayed by the system
• AT 100’ requires natural view of visual references
• Controlling RVR is reduced by
RVR/CMV Normally required
RVR/CMV for approach utilising EVS
550 350
600 400
650 450
700 450
Example RVR Reduction
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Rockwell Collins Proprietary Information
• Controlling RVR is reduced by approximately 1/3
700 450
750 500
800 550
900 600
1000 650
2000 1300
3000 2000
4000 2600
4
Enhanced Flight Vision System (EFVS) Today
• Technical Solution Today: Extended mid-IR Camera systems– Operates in the ~1 to 5 micron band (cooled InSb cameras)
• Two EVS sensor suppliers: Kollsman and CMC
• Today’s Sensors meet certification requirements
– Displayed Head-Up
– Can Detect “airport environment” above 200’ in many
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Rockwell Collins Proprietary Information 5
– Can Detect “airport environment” above 200’ in many environments
– Adequate latency and resolution
• Issues with Today’s Sensors
– Not sensitive to evolving LED-based airfield lighting systems
– Reliability
– Size and Weight
– Cost
Visible and Infrared Spectrum
SWIR LWIRMWIR
EVS Sensor Spectral Ranges
Visible
Extended MWIR Today’s Sensors
© 2015 Rockwell Collins. All rights reserved.
Rockwell Collins Proprietary Information
LED
Incandescent, Halogen LightsRunway Thermal
Background
© 2015 Rockwell Collins. All rights reserved.
Rockwell Collins Proprietary Information
ROCKWELL COLLINS APPROACH
Rockwell Collins EVS-3000
• Entry into service in 2015
– Embraer Legacy 450 / 500
• Multi-spectral technology
– High resolution image across broader spectrum
– Includes LED detection necessary for lower operating minima
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Rockwell Collins Proprietary Information
• Uncooled sensor
– Higher reliability
– Lower size, weight and power
– Lower cost than current generation EVS for credit
• Availability on additional aircraft expected after initial EIS
8
Visible and Infrared Spectrum
SWIR LWIRMWIR
EVS Sensor Spectral Ranges
Visible
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Rockwell Collins Proprietary Information
LED
Incandescent, Halogen Lights Runway Thermal Background
FY15 Planned spending Profile
HGS™ at night with EVS-3000 (actual flight)
EFVS effective at and in (some) weather…..
Today, EFVS isFAA-approvedto replace naturalpilot vision from
© 2014 Rockwell Collins All rights reserved.
Rockwell Collins Proprietary Information
pilot vision from200’ to 100’ AGL.
Rulemaking inprogress forapproval to touchdown.Equivalent Visual Operations…Except for weather that cannot be penetrated by inf rared.
EVS-3000 Flight Test Video
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Rockwell Collins Proprietary Information 11
FY15 Planned spending Profile
Building up an Equivalent Visual Operation
© 2014 Rockwell Collins All rights reserved.
Rockwell Collins Proprietary Information
200’AGL
100’AGL
50’AGLTD
1200’ 1200’
FY15 Planned spending Profile
Building up an Equivalent Visual Operation
© 2014 Rockwell Collins All rights reserved.
Rockwell Collins Proprietary Information
200’AGL
100’AGL
50’AGLTD
1200’ 1200’
150’AGL
SYNTHETIC VISION SYSTEMS
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Rockwell Collins Proprietary Information 14
Head-up Synthetic Vision System (SVS)
Innsbruck Approach• Computer generated real time view of the
world from a pilot’s perspective based on terrain, runway, and obstacle databases
• Enhances awareness of the aircraft’s position relative to the runway and surrounding terrain
• Three discrete database “layers”
• Certified on BA Global Express
• SVS for lower landing credit (150’ DH,
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Night w/ HUD HUD w/ SVS
• SVS for lower landing credit (150’ DH, 1500’ RVR) in process
SVS Video
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Rockwell Collins Proprietary Information 16
FY15 Planned spending Profile
Building up an Equivalent Visual Operation
© 2014 Rockwell Collins All rights reserved.
Rockwell Collins Proprietary Information
200’AGL
100’AGL
50’AGLTD
1200’ 1200’
150’AGL
COMBINED VISION SYSTEMS
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Rockwell Collins Proprietary Information 18
Head Up Vision System – Combined Vision
SVGS is weather independent, but limited by accuracy of navigation solution and integrity of databases
– Independent monitoring solutions will enable SVGS approaches to 1400RVR / 150’ DA
EFVS performance weather dependent
– Sensor must image at Decision Altitude allowing the pilot to fly the Visual Segment from the standard DA/DH to 100’ HATh, or the runway (depending on EFVS I or II system)
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Rockwell Collins Proprietary Information 19
HATh, or the runway (depending on EFVS I or II system)
• Combines the operational credits associated with EFVS and SVGS and seamlessly connects these technologies to increase operational reliability
– Adaptive Smart Fusion algorithm blends based on image detail
• HVS Technology Focus:
– Continued focus on best integration of technologies
– Drive subsystems to right cost/performance point
– Develop new technologies that increase operational benefits.
– Develop algorithms for image optimization minimizing clutter and ensuring system enhances natural visibility
FY15 Planned spending Profile
CVS on HGS™ at 1400’ AGL
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Rockwell Collins Proprietary Information
FY15 Planned spending Profile
CVS on HGS™ at 860’ AGL
© 2015 Rockwell Collins. All rights reserved.
Rockwell Collins Proprietary Information
FY15 Planned spending Profile
CVS on HGS™ at 640’ AGL
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Key Benefits of CVS
1. The fused image is better than the sum of its parts� Single HUD image contains key information from multiple sources
2. Reduced cockpit workload� Imagery is easily interpreted, more timely situational awareness
3. Information content highly adaptable to current operation� Take-off, climb and cruise, approach and landing, roll-out, taxi
© 2015 Rockwell Collins. All rights reserved.
Rockwell Collins Proprietary Information
� Take-off, climb and cruise, approach and landing, roll-out, taxi
� Automatic or manually tailored (pilot selectable modes?)
4. Improved system integrity and certifiability� Sensed and Synthetic streams are derived from independent and
dissimilar sources
� Comparisons lead to higher Design Assurance Level, and eventually to improved operational benefits
� Additional Landing Benefits
Combined Vision System
SVS
Integrated Head Up / Combined Vision
HVS Key Functions:• Integration point for all sources
of real time video vision data • Selectively fuses video to
provide “best view” in all conditions
• Goal: “VMC” operations in all environmental conditions
• Certification target: 300 RVR by 2020
“Best View”
HUD System
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Rockwell Collins Proprietary Information 24
Enhanced Vision Sensors(Visible, SWIR, LWIR)
Active RF systems (ESA radar, mmw)
Combined Vision System Processor
Ambient vision
“Best View”
Heads-Up, Eyes Out Operations