Abstract

Degraded Visual Environment (DVE) is experienced when helicopters enter Inadvertent Instrument Meteorological Conditions (I-IMC). DVE can occur in the form of fog, night flight occurring naturally or when pilots try to land in unprepared (dusty, snowy) landing zones causing brownouts and whiteouts from rotor downwash. The Degraded Visual Environment Navigation Support (DVENS) project aimed to use a LiDAR to scan a specified Field of View (FOV) and range to identify a zone to be safe or unsafe for landing in a simulation capacity. A Head Down Display (HDD) with touch capabilities was used to provide Virtual Visual Meteorological Conditions (V-VMC), in which 3D conformal, 2D orthographic symbology is displayed. For the iterative design of the symbology, to diagnose and minimize pilot error in DVE the Taxonomic Framework for Aircrew Error evaluation is used. The framework allowed for a more direct design approach with clear objectives based on operational requirements and presenting an optimal workload for pilots. Maintaining the objective of showing the required information to the pilots while minimizing clutter is imperative as too much information can increase workload. Thus, the aircrew error Taxonomic framework helps identify the design goals required to neutralize pilot error leading to an efficient design. The Ryerson Mixed Immersive Motion Simulation (MIMS) lab’s Fixed Base Simulator (FBS) and CAE, Presagis’s HELI CRAFT were used as the simulation testing tools. Non-intrusive questionnaires such as NASA Task Load Index (TLX), Bedford and Cooper-Harper display rating scales were used to provide feedback and evaluate the display system. Multiple scales were used for validation of results and to measure the workload, stress, physical, psychological and time loads. This methodology and design were found to be extremely helpful in assisting pilots to land, take off in DVE and IIMC conditions.

Highlights

  • Degraded Visual Environment (DVE) is experienced when helicopters enter Inadvertent Instrument Meteorological Conditions (I-IMC)

  • In the scenario that Degraded Visual Environment Navigation Support (DVENS) system signifies an area as safe to land over a specified range, the pilot can select a zone by touch capability, where 3D world conformal symbology would be displayed to help them land providing virtual cues for situational awareness

  • This project provides a fusion of incoming Light Detection and Ranging (LiDAR) data and updates it in real-time with pre-loaded Digital Elevation Map (DEM) on the backend level with a symbology displayed in the front end

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Summary

HELICOPTERS AND DOWNWASH

The first active operational helicopter was the German Focke-Wulf FW 61 which flew in 1936, which was later developed into many other designs. The primary cause of brownouts and whiteouts in helicopter operations occur in unprepared landing sites due to helicopter downwash [3]. Police and military helicopters must be available around the clock in any weather or environmental conditions and their operation cannot be hindered due to DVE or weather anomalies [3]. With their ability to hover and Vertically Take-Off and Land (VTOL), helicopters see a broader range of operational environments and mission scenarios compared to fixed-wing aircraft. Their ability to perform such dynamic roles, allow them to operate in unprepared and undeveloped areas. Class A accidents are damages of property over $2 million and class B are damages costing between $500,000 and $2 million suffered by the US Military [6]

OBJECTIVE DEFINITION
RESEARCH TOOLS
PROBLEM-SPECIFIC STUDY
SITUATIONAL AWARENESS AND ILLUSIONS IN AVIATION
Autokinetic Illusion
HELICOPTER OPERATIONS AND MANEUVERS
Landing Procedure
HELICOPTER FLIGHT DECKS, PAST, PRESENT AND THE FUTURE
Engine Backup systems
SPECIFIC TO THE DVE SOLUTION
Performance Instruments
Navigation Instruments
SECONDARY VIEW MODES AND TERRAIN TEXTURES The basis of Situational
HUMAN CENTERED DESIGN
EVALUATION METHODS
SYMBOLOGY REQUIREMENTS BASED ON FLIGHT CONDITIONS
Ground slope
Terrain Features
Landing Point Location
HELICOPTER REFERENCED INFORMATION
DESIGN OF SYMBOLOGY BASED ON ERROR TAXONOMY
TERRAIN TEXTURE REPRESENTATION
FILTERING DATA SOURCES
NAVIGATION VIA WAYPOINTS AND LANDING ASSIST
FLIGHT PARATMETERS AND TRANSISIONS
AUXILLIARY SYMBOLOGY
FINAL SYMBOLOGY
FLIGHT AND TEST PLAN
TABULATION AND EVALUATION OF RESULTS
NON-INTRUSIVE QUESTIONNARIE RESULTS
Landing Accuracy Results for PFD landings
SUMMARY AND DISCUSSION
FUTURE WORKS
Full Text
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