History
of UAS
Early
Design: Ryan Model 147
The U.S. Army Ryan Model 147 “Lightning Bug”, derived
from the early Firebee model, was in use from 1965 to 1975 and performed over
3400 reconnaissance missions (Blom, 2010). Most of these sorties were flown
during the Vietnam War, where the Lightning Bug conducted visual and electronic
signals intelligence gathering in both high and low altitude regimes. During
the operational periods where the 147 was used, flight programs were uploaded
nearly two weeks prior to launch and the only changes that could be made in the
field were wind calculations (Blom, 2010). Many of the unmanned aerial vehicles
(UAV) crashed, were subject to critical navigation errors, made unpredicted
turns, and some even failed to switch to remote control prior to landing and
would fly until running out of fuel (Blom, 2010).
Contemporary
Design: MQ-1 Predator
The MQ-1 Predator is a widely recognized, capable and
proven UAS that is undoubtedly a predecessor of the infamous “Firebee” and
“Lightning Bug” aerial vehicles (Ehrhard, 2010). Initially designated as RQ-1
in the late 1990’s, the Predator has evolved into a multi-mission platform
capable of intelligence, surveillance and reconnaissance (ISR) missions, laser
designation, and air-to-ground strikes (Clausen, 2016). The Predator is able to
execute pre-programmed flight routes, gather and send near real-time data feeds
to operators, and safely conduct launch and recovery evolutions at an airfield
or prepared surface using remote control or automated sequences (Clausen, 2016).
Comparing
and Contrasting the Designs
Designing variants and types. Typically with modern UAS, there are only a few variants of the same
platform operational and development of new variants take significant amounts
of time, however the 147 underwent a very rapid and “ad-hoc” development scheme
to improve performance and make design changes. Figure 1 below illustrates the
timeline of the changes made to the 147 airframe, with mission capabilities
building over time. Additionally, instead of developing system enhancements and
adding them to the existing airframe, Ryan engineers decided to make specific
variants that were only used for certain missions and conditions. For example,
cloud cover was obscuring image quality and degrading the photo capabilities
for the Bravo variant, but the Charlie variant hosted a new technology to fly
at low altitudes called the barometric low altitude control system (BLACS) (Ehrhard,
2010).
The level of control between the 147 and MQ-1 is
different, in that the 147 had a “fire and forget” mentality where the UAV
would be launched, and once it would return (or be recovered) then the data
would be extracted and later analyzed. In terms of the MQ-1, the level of
human-to-machine interface has greatly increased, with remote ground stations
able to process the data feed and make rapid tactical decisions based on the
ever changing battlespace environment (Clausen, 2016).
Launch and recovery. At
the most basic level, the method of launch and recovery is vastly different when
comparing the two airframes. With the Lightning Bug, a C-130 airframe would
airlift the drone to a prescribed altitude and then release it, or would
utilize jet-assisted takeoff (JATO) boosted capabilities from a land-base or
ship (Blom, 2010). The reliability rates for a successful landing or recovery
for the 147B model was approximately 62%, whereas the MQ-1 utilizes much more
refined automated landing sequences with better global positioning system (GPS)
fidelity to execute a more accurate and consistent recovery (Ehrhard, 2010). As
the systems evolved, the needs for fulfilling mission requirements (i.e.
overcoming cloud cover, launch and recovery constraints, better communication
systems) became more clear, and the Lightning Bug paved the way for future UAS
programs. The early programs provided the benefits of ad-hoc engineering
design, valuable lessons learned for launch and recovery operations, and the
need for rapid delivery of flight telemetry and intelligence data using
sophisticated communications networks (Ehrhard, 2010). Determining the need for
refining telemetry based on the early drone experimentation with altimeters,
timer-programmers, and gyrocompasses enabled future UAS programs to develop a
better navigation system which aided in higher vehicle recovery success rates
(Ehrhard, 2010).
Figure 1. Ryan Model 147 Variants List. Retrieved from unmanned
aerial systems: a historical perspective. Copyright US Army Combined Arms
Center, 2010.
Influencing
the Future based on New Technology
New technology such as wireless energy transfer using line of
sight (LOS) systems can greatly increase the payload capacity for each
airframe, in that extra space and storage previously occupied by heavy
batteries and/or jet propulsion can be used for adjunct sensors (Morris, 2016).
Additionally, when considering the use of power transmission over
short-ranges, the capacitive power transmission (CPT) yields advantages such as
minimizing the problem of electromagnetic interference (EMI) and greatly
reducing power losses due to the operating environment (Mustafa, Muharam &
Hattori, 2017). This new technological enhancement that allows for more usable
space on UAS yields some distinct advantages that might influence the future
evolution for UAV design. System enhancements would also need to be made to the
ground stations to monitor power transmissions, and ensure that LOS is
constantly maintained in order to provide adequate power for the vehicle under
all operational conditions/flight regimes.
References
Blom,
J. D. (2010, September). Unmanned aerial systems: A historical perspective. Aerial Reconnaissance: Drone Aircraft, 2(37),
1-353.
Clausen, C. (2016, December 15). The evolution of the combat RPA. Retrieved from
http://www.acc.af.mil/News/Article-Display/Article/1031490/the-evolution-of-the-combat-rpa/
Ehrhard, T. P. (2010, July). Air Force UAV’s: The secret history. Retrieved from http://www.dtic.mil/dtic/tr/fulltext/u2/a525674.pdf
Morris, D. Z. (2016, September 24). Demo shows drone flying under wireless power. Retrieved from http://fortune.com/2016/09/24/drone-flies-wireless-power/
Mostafa, T. M., Muharam, A., & Hattori, R. (2017, May
20). Wireless battery charging system
for drones via capacitive power transfer. 2017
IEEE PELS Workshop: Emerging Technologies – Wireless Power Transfer. doi: 10.1109/WoW.2017.7959357
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