Sunday, August 23, 2015

Weeding Out a Solution- A Systems Engineer in Action


As a systems engineer I would be modestly irritated that my teams did not follow parameters that were set forward as part of the design process. To best convert a marketing concept into a real life system, wish lists dreamed up by high level management (or high level requirements) must be broken down into more design specific instructions (Lowen, 2013). Design teams depend on these decomposed instructions (or low level requirements) to develop the UAV (Lowen, 2013). In a requirements based design process, special care is taken to drive a high level description of the design through to the implementation details (Lowen, 2013). In essence, this high level requirement is transformed into a list bulleting what is needed on a technical level to carry out the exact system feature (Lowen, 2013). When we began to exam this particular UAV it should be noted that the design team failed to hit the checks in the box when they began going over budget. One of the big flaws in this design was exactly that, the budget, naturally having the marketing team hype up something and not being able to deliver on that is costly. Things that we have to consider in this design is what the customer wanted, they wanted a system that could fly correctly, and secondly that the system would spray correctly. These considerations become top priority or “high level requirements,” and because the teams have failed to realize this at the lower level we now have a system that risks being unsafe and cuts into the fuel margin.  
This brings me up to how things should have been conducted leading to a much different result. The main focus should be on decision management. While there are many other important roles that come to be a factor in systems engineering, in this instance, the “Great Decider” role plays perhaps the most critical. As the lead systems engineer I would have implemented design objectives. The first step is to develop objectives and measures using interviews and focus groups with subject matter experts (SMEs) and stakeholders ("Decision Management"). For systems engineering trade-off analyses, stakeholder value often includes competing objectives of performance, development schedule, unit cost, support costs, and growth potential("Decision Management"). For corporate decisions, shareholder value would also be added to this list ("Decision Management"). For performance, a functional decomposition can help generate a thorough set of potential objectives ("Decision Management"). For each objective, a measure must be defined to assess the value of each alternative for that objective. A measure (attribute, criterion, and metric) must be unambiguous, comprehensive, direct, operational, and understandable ("Decision Management").  Once we have established our value based objectives it would then be time to start coming up with designs that would fit those parameters along with alternative designs that could work. After all of those details have been ironed out, we would have a set of possible designs with one of the systems meeting more requirements than the others.            
As the great decider I would have the opportunity to choose the design that best met our customer’s request. Rather than come up with a design that was costly and tried to cut corners by using commercially off the shelf products, we could have seen the reward in designing a custom built UAV to meet customer requirements. So for the next generation enhanced version of this UAV it may be more costly because of its custom nature, but it would certainly get the job done without much in the way of being overweight. As newer technology became available, or once the system was realized for its useful potential, products that were customized then could become a viable commercially off the shelf product.
References
Decision Management. (2015, June 16). Retrieved August 23, 2015, from http://sebokwiki.org/wiki/Decision_Management

Lowen, H. (2013). Requirements-based UAV Design Process Explained. Retrieved August 23, 2015, from http://www.micropilot.com/pdf/requirements-based-uav.pdf

Sunday, August 16, 2015

Gyrodyne DASH vs. Northrop Grumman Fire Scout

                              When we review the history of unmanned aircraft systems one particular concept that has carried through the age of time was the introduction of a “battlefield UAV.”  The first one of its kind was the Gyrodyne DASH. It was a dedicated design for the purpose and not a development of a target system. Its task was to fly from US Navy frigates and to carry torpedoes or nuclear depth charges to attack enemy submarines that were out of range of the ship’s other weapons. In terms of control systems, it could be considered a backward step since it carried no autopilot or sensors, being merely radio controlled and, presumably radio or radar-tracked for positioning (Austin, 2010). It did, however, introduce a different role and for the first time the use of a rotorcraft UAV. One could argue that the invention of this “battlefield UAV” led to the introduction of other battlefield systems. The unmanned aircraft with the most similarity is the Northrop Grumman Fire Scout. The Fire Scout is a fully autonomous, four-blade, single-engine unmanned helicopter. Fire Scout supports both maritime- and land-based missions, taking off and landing on suitably equipped air-capable warships and at prepared and unprepared landing zones. The MQ-8C has been designed to communicate easily with shipboard controllers using the Navy’s Mission Control System ("MQ-8C Fire Scout Unmanned Air System").
            One of the main problems with the DASH was the lack of a "feed-back-loop" from the drone to the controller which prevented the operating drone controller from knowing the drone's orientation. This was exacerbated by the low radar profile of the QH-50 (DASH) to the ships tracking radar and the lack of transponders resulted in the loss of many drones due to not knowing WHERE the drones were in relation to the ship ("DASH History"). Because this system was Non-Redundant, once communication was lost with the UAV, the system itself was lost. Because of this lack of redundancy there needed to be a design that incorporated various levels of redundancy in addition to this, a better onboard communication system between the UAV and the ship’s communication. This new system is what we see on many of today’s naval vessels which is called the Mission Control System. This new system created a system oriented architecture for use on ships, which eventually led to the invention of the Broad Area Maritime Surveillance system or BAMS. This BAMS is utilized by the Triton Unmanned aircraft and has been an extremely valuable asset.
            These two systems are similar not only in the fact that they are both rotorcraft, but their missions are eerily the same, they both utilize a COTS approach, and both use a form of radio communication. Where they differ is technology, redundancy, and autonomous capability.  The Fire Scout comes equipped with a TCDL (tactical common data link), a UCARS (UAV Common Automated Recovery System), modular payloads, and a more sophisticated mission control system ("MQ-8B Fire Scout Brochure"). Without the early failures of the DASH program, it would be hard to say if this system would be in use. The initial concept of using a VSTOL “battlefield UAV” was a great idea, but the lack of a sophisticated control station in conjunction with poor radio communication, and lack of redundancies, the DASH program was retired, which ultimately led to the need for a more sophisticated system that could do the same mission of DASH, but do it better with less loss of aircraft.  These failures led to a need for a redundant system and eventually the creation of a VTUAV (vertical Takeoff/landing tactical unmanned aerial vehicle).

              

FIRE SCOUT

Gyrodyne DASH






















References
Austin, R. (2010). UAV Systems Continuing Evolution. In Unmanned air vehicles UAV design, development, and deployment (Kindle ed., pp. Location 8656-9018). Chichester, West Sussex: Wiley.
DASH History. (2013). Retrieved August 16, 2015, from http://www.gyrodynehelicopters.com/dash_history.htm
MQ-8B Fire Scout Brochure. (2010, February 8). Retrieved August 16, 2015, from http://www.northropgrumman.com/Capabilities/FireScout/Documents/pageDocuments/MQ-8B_Fire_Scout_Brochure.pdf
MQ-8C Fire Scout Unmanned Air System. (2015, April 1). Retrieved August 16, 2015, from http://www.northropgrumman.com/Capabilities/FireScout/Documents/pageDocuments/MQ-8C_Fire_Scout_Data_Sheet.pdf