Tuesday, December 6, 2016

UAS GCS Human Factors Issue Assignment 2.5 ASCI 638

Human factors of MQ-5B Hunter
Scott E. Leishman
ASCI 638- Human Factors in Unmanned Aero Sys
Assignment 2.5
Embry-Riddle Aeronautical University-Worldwide
November 29, 2016

Unmanned Aerospace system
For this assignment I chose the MQ-5B Hunter. This tactical Unmanned aircraft system is a long endurance, medium altitude multi-mission (UAS). In particular this UAS was enhanced to provide the Army with a steadfast aircraft that was capable of keep constant Intelligence, Surveillance, and Reconnaissance (ISR) in the battlefield. The MQ-5B conducts battlefield surveillance using multiple sensors, including its multi-mission EO/IR/LD/LRF/Illuminator and Signal Intelligence (SIGINT) payloads ("MQ5B Hunter-Capabilities"). This system utilizes JAUS or Joint architecture for unmanned systems. JAUS is a common language enabling internal and external communication between unmanned systems.
Common architecture and elements. This UAS employs a GCS-3000 ground control station (GCS) which is typically manned with two operators (A pilot and a sensor operator/navigator). It allows the UAS to track, command, control and communicate with not only the air vehicle but the payloads onboard as well. The GCS is capable of controlling up to 2 air vehicles at a time using one GCS. The GCS comes equipped with a digital terrain and elevation data, as well as CD ROM map data and data from the Defense Mapping Agency (DMA) ("Hunter RQ-5A / MQ-5B/C UAV, United States of America"). 
Command and control strategy. This unmanned air vehicle can operated either from a paved or a semi-paved runway or can be launched via a rocket assisted takeoff system (RATO).  The RATO launch is useful on board small ships and in areas where space is limited. This UAS has an automated takeoff and landing component to it and the GCS is setup in four bays. The four bays are as follows: Pilot bay(controls flight of UAS),  Observer bay (payload functions), and a Navigation bay, which has a digital map display which will trace the flight path and monitor mission progress and finally the intelligence pay which incorporates data processing and distribution capabilities. ("Hunter RQ-5A / MQ-5B/C UAV, United States of America"). Northrop Grumman data sheet dictates the main logic controller for this system is the BLK II OSGCS (One station ground control system) with ATLS (automatic takeoff and landing system). With the OSGCS, vehicle control station software is installed and allows for more automation in flights, in particular this UAS is equipped with VCS-4586 which according to Lockheed Martin  “Operators enjoy real-time control and monitoring capabilities through an intuitive point-and-click user-interface requiring only a keyboard and mouse (Lockheed Martin, 2016).”
Human factors issues
            Although this UAS has performed over 80,000 hours of operations, it still has human factors issues at play within the GCS. One of those issues is automation. While automation is one way to negate over saturating a task, it also eliminates common skills that are retained through constant use, i.e. piloting. Take this particular UAS, if for some reason any part of the communication link were to fail, and the GCS was no longer automated, the pilots would have to intervene, and if they forgot how to do something that is typically routine, for example landing, the results could be disastrous. To negate this issue, pilots should be able to override automation, and should balance automation with level of saturation. If the pilot has too many mission tasks, they should employ automation, but in the event that the pilot is only doing routine operations, automation should be limited to when the UAS is loitering or in times where pilot intervention would infrequently be needed. Another perceived human factor issue is displayed information used for this UAS within the GCS. While it is good to have access to as much information as possible, sensory overload can be another factor. This GCS could benefit from having a multimodal display that would advise pilots of important information. This would be extremely useful in events where an aircraft operated in instrument meteorological conditions (IMC) or near IMC.
Conclusion
When we consider a design for a UAS and important functions for the GCS, every characteristic of that system should be properly evaluated to determine what the most effective and efficient roles are for the human operator and machine (Hunt, Rice, Geels, & Davis, 2012). We should assure that automation is not to exceed a level where the human operator can no longer operate the aircraft, but not take away automation to a point where the operator loses the ability to multi-task and take away from mission goals. Additionally, the flow of information is a crucial aspect of operating an aircraft properly. The flow of information needs to be widely understood by any and all individuals involved with that system and it should be effective and efficient as possible (Hunt, Rice, Geels, & Davis, 2012). Finally, the attributes of the hardware and software available between the man-machine interfaces should take into consideration how the users will interact with that technology. In addition to understanding the interaction between the hardware, software and human-machine interface, special attention should be given to possible lag times and other potential issues with the given technology suite(Hunt, Rice, Geels, & Davis, 2012).


References
Hunt, G., Rice, S., Geels, K., & Davis, D. (2012). Using Magpie Research to Determine the Top 10 Human Factors Issues in UAS for NATO FINAS. Proceedings Of The Human Factors And Ergonomics Society Annual Meeting, 56(1), 1524-1528. http://dx.doi.org/10.1177/1071181312561303
Hunter RQ-5A / MQ-5B/C UAV, United States of America. (n.d.). Retrieved November 29, 2016, from http://www.army-technology.com/projects/hunter/
MQ5B Hunter-Capabilities. (n.d.). Retrieved November 29, 2016, from http://www.northropgrumman.com/Capabilities/MQ5BHunter/Pages/default.aspx
MQ5B-Datasheet. (n.d.). Retrieved November 29, 2016, from http://www.northropgrumman.com/AboutUs/BusinessSectors/TechnicalServices/Documents/MQ-5B_Hunter.pdf
Lockheed Martin,. (2016). Retrieved 30 November 2016, from http://www.lockheedmartin.com/us/products/cdl-systems/VCS.html


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