A UAS is to be
designed for precision crop-dusting. In the middle of the design process, the
system is found to be overweight.
Two subsystems – 1)
Guidance, Navigation & Control [flying correctly] and 2) Payload delivery
[spraying correctly] have attempted to save costs by purchasing off-the-shelf
hardware, rather than a custom design, resulting in both going over their
originally allotted weight budgets. Each team has suggested that the OTHER team
reduce weight to compensate.
The UAS will not be able
to carry sufficient weight to spread the specified (Marketing has already
talked this up to customers) amount of fertilizer over the specified area
without cutting into the fuel margin. The safety engineers are uncomfortable
with the idea of changing the fuel margin at all.
Write a response
describing how you, as the Systems Engineer, would go about resolving this
issue. Use your imagination, and try to capture what you would really do. Take
into account and express in your writing the things you’ve learned so far in
this module: What are your considerations? What are your priorities? What do
you think about the future prospects for the “next generation, enhanced”
version of the system as a result of your approach?
While it is important that the vehicle both fly correctly
and spray correctly there needs to be a solution to the overweight
dilemma. Reducing the weight of unmanned
aerial vehicles (UAVs) pays large dividends in their ability to carry more
fuel, support more advanced payloads (radar, imaging, sensors, navigation and
guidance, uplinks and downlinks), achieve longer flight times, and operate from
shorter runways (Oliver, 2012). Both
teams have decided on using off-the-shelf (OTS) hardware which has resulted in
an overweight situation. The fixed
factors are the fuel and the amount of fertilizer. Therefore, the only manageable means of
navigating this situation is to design custom lighter options for guidance,
navigation & control, payload control, increase propeller lift capability,
increase motor size, or utilize a lighter design structure for the entire
craft.
In most design projects it comes down to two very important
factors; time and money. Therefore, I
will begin this project by mandating that each team compile a report that
specifies the time and money required to design a custom solution instead of
the OTS version. By forcing the teams to
figure out a solution within the design parameters, it will encourage
creativity and possibly flush out new ideas or theories that can lead to
breakthrough solutions. The best case
scenario is that one or both teams find an easy solution to the weight problem
by either slightly modifying the OTS version or designing a new version that is
within cost, time, and weight parameters.
Reducing the weight of the
electronics, and especially the power-supply subsystem, is a major area for
potential improvement (Oliver, 2012).
Meanwhile, I will consult the propulsion department and have
that department begin an evaluation to determine if a different type of
propeller is capable of carrying the weight with no negative fallout in regards
to the fuel or time aloft considerations.
If the propulsion department cannot produce a better lifting mechanism I
will suggest investigating a larger power source. However, I will stress that the power source
must not use any more fuel than what is currently allotted per the original
design specifications.
Lastly, consulting with the structure design engineers may
result in some ideas that will result in a lower overall weight to the
vehicle. I will encourage they
investigate other materials that may be more durable and lower weight. However, the cost consideration along with
ability to procure material will need to be considered as part of the overall
project goals and objectives.
Ultimately, both teams have failed to fully analyze the
problem and create a solution within their parameters which is unacceptable for
the success of the project. They need to
go back to the drawing board and come up with custom intelligent designs that
meet the demands of the project, thus keeping the project on track. However, if neither team is able to
accomplish a better solution than the OTS, I have consulted with other
departments that might be able to offer a solution to the overweight
problem.
REFERENCES
Oliver, S. (2012, August). Take A Multifaceted Power
Approach To Reduce Your UAV’s Weight: Electronic Design. Retrieved from http://electronicdesign.com/power/take-multifaceted-power-approach-reduce-your-uav-s-weight
Chris,
ReplyDeleteGreat blog and post!