UAS in the National
Air Space
Integrating UAS in
the National Air Space has been ongoing for a number of years. Despite everyone’s best interest to move the
subject forward in an expeditious manner, it is not so easy. The Federal Aviation Administration is
deliberate in their approach, despite Congress and the private sector exerting
pressure. At the AUVSI Xponential
Conference in New Orleans this year, Michael Huerta, the FAA Administrator
stated that the United States Government is committed to the integration of UAS
in the NAS through a series of efforts that involve all interested parties
(AUVSI, 2016). FAA’s goal is to first
accommodate, then integrate and evolve unmanned aerial systems into the
National Air Space (UAS Integration, 2012).
In that effort, the focus is to first accommodate the small UAS. This paper discusses actions taken by the
U.S. Government to permit small UAS in the NAS, and how it is addressing the
separation of unmanned and manned systems. FAA’s Section 333 Exceptions and Part 107
Small UAS Rules are the first attempts to address varying sizes and types of
airframes. It may serve as an example of
how it intends to address larger sizes and types of aircraft.
While government
action through laws and regulations are important, there are significant technical
challenges. The National Air Space is
regulated by manned flight. These
regulations are well established and serve their purpose in an efficient matter
to ensure the safety of flight. Integrating
UAS in this environment presents challenges that with time will be
resolved. There exist manned aircraft
technologies that can apply to the UAS community. This paper will discuss existing technologies
that apply today, which may be relevant to assist in integrating larger unmanned
airframes into the NAS.
Efforts for Separation of Aircraft
FAA’s current
efforts with the introduction of Section 333 Exception and Part 107 Small UAS
Rule are examples of how to accommodate unmanned system by allowing them to fly
in designated areas. Under a Section 333
Exception UAS can fly with a Certificate of Authorization in areas designated
by the FAA as exclusive for the use of unmanned systems. Part 107 allows flight
with and without concurrence from the Air Traffic Controller for the area of
operation depending on the airspace class (Section 333, n.d.; Operation and
Certification of Small UAS, 2016).
The intent of the rules
for small UAS (less than 55 Kg) is to permit operations in Class G airspace
below 400 feet where the expectation of a manned aircraft in that space is
unlikely. However, the existing rules
allow permission in the Class B, C, D and E airspaces with the ATC’s
permission. These are the first steps to
allow operation with an effort for separation of aircraft.
For UAS desiring
to fly about 18,000 feet in the NAS, Huerta stated at the AVUSI Conference that
under the existing rules, it must meet manned flight requirements to include
sense and avoid. FAA understands that it
must resolve how it will handle is part of the airspace, because it will have a
significant economic impact if not resolved.
The FAA has created a broad-advisory committee to advise policymakers of
UAS integration, which will address these issues.
There is a
significant gap between the operation of larger UAS (greater than 55 Kg) and
flying above the 400 feet below 18,000 feet.
One would assume that the FAA is working with industry and other stake
holders through the Advisory Board that will make recommendations to permit the
use of this airspace without the current laborious task encumbered by the
Section 333 Exceptions process. Unlike
the small UAS Part 107 rules, it may include technology solutions in addition
to procedural requirements. The way Part
107 rules our structured provides the hint that the direction FAA may take with
regard to the operating of larger airframes in the 500 to 18,000 feet airspace. The comments that the requirement under Part
107 are waivable by FAA if the applicant can demonstrate that safe operation
can be conducted via a certificate of waiver.
These comments are welcomed. By
stating that waivers will be considered upfront, it shows that FAA is trying to
accommodate the UAS, vice putting them in a box where it would difficult to fly
in the NAS to provide services in the commercial market.
Considerations for varying sizes and
airframes of UAS
Sizes
and types of airframes do make a difference.
FAA recognized the issue and properly decided to implement Part
107. There was no need to restrict the
use of small UAS, if there was not an imminent threat to the manned aircraft,
particularly since manned aircraft should not fly less than 1000 ft. In establishing the 400 feet limit, it also
established a buffer between the two types of aircraft.
For
the larger airframes, Section 333 Exceptions provides a method to allow
operations. The operating rules and
aircraft requirements are similar to Part 107, with the pilot requirement being
evaluated by the FAA on a case-by-case basis (Beyond the Basics, 2016).
If
the type of airframe is unique such as an aerostat, the process is still the
same. The operator must obtain a
Certificate of Waiver or Authorization just as it was a fixed or rotary wing
asset. In the author’s previous experience aerostats in the United States,
coordination with the local ATC was required above 1000 feet for an approved
COA.
Manned Aircraft Technologies Adaptable for UAS
Manned
aircraft are equipped with several technologies that are adaptable to the
unmanned aerial system. Some can be
installed in the larger Group 4 and 5 airframes. Some of the systems can be modified into
smaller form factors that may work with the unmanned system. For the smallest
UAS, these systems are not sized to fit within the airframe, or are not
economically feasible to be integrated into the smaller systems. As discussed in the previous section, there
needs to be considerations made because for some of the UAS having equivalent
systems to manned aircraft is not feasible.
Even within the manned aviation aircraft, it may or may not have some of
the components listed in this section.
Clot
(n.d.) provides a detail listing of the most commonly used systems onboard an
aircraft that are pertinent to adapting to unmanned system for acceptance into
the NAS. The equipment include navigational
and surveillance systems. Listed below
are the more pertinent systems that could be used for UAS.
Navigational Systems
Most
of the navigational system used onboard a manned aircraft are for the pilot to get
reference of his position relative to stationary beacons or airport
towers. If they are operated by the UAS pilot,
they can be useful in confirming the position of the vehicle in the NAS. These include a VHF Omni-Directional Radio
Range (VOR), a Distance Measuring Equipment (DME), a Tactical Aid to Navigation
(TACAN), Instrument Landing System (ILS), Microwave Landing System (MLS). While they may be practical for manned flight
and specific unmanned system, one would have to evaluate the benefits of one
over another for the specific application.
For example, onboard US Navy ships, TACAN is an important navigational
aid. Most U.S. Navy warships have this
system onboard. For an unmanned system
operating from an naval ship, the use of TACAN could be important in the
recovery of the vehicle.
There
are two navigational systems that are used in manned aircraft that are also
used in unmanned systems, GPS and Internal Navigation Systems (INS). Both are important for the safe operation of
aerial vehicles in the NAS. With the
additional of one or more of the navigational system noted above, one can be
confident that the location of the unmanned system is known to the operator,
and could be transmitted to the local ATC.
Surveillance Systems
There
are several systems used to exchange information between the manned aircraft
and the ground. Some of these system
include radars, data exchange, and collision avoidance systems. Each one can serve the unmanned community in
assisting the integration of the vehicle into the NAS. Secondary Surveillance Radars have
identification system that sends out a signal to interrogate each aircraft
within sight of the radar. The aircraft
will then send its position (Mode A) and its altitude (Mode C).
When radar is not
available information from the aircraft is shared with an Air Traffic Control
Center via the Automated Dependent Surveillance (ADS) System. These messages sent by the aircraft to
satellites can also be received by anyone with a ADS receiver. This could be an
important addition to any UAS, in particular those flying above 18,000 feet.
The Tactical
Collision and Avoidance System (TCAS) is a new component that exchanges
information between aircraft and the ground.
It alerts manned aircraft of other aircraft near them. This is clearly a technology that will help
UAS integrate into the NAS in the near future.
Conclusion
The integration of
UAS into the National Air Space requires laws, regulations, procedures and
technology. A combination of these
elements will eventually allow the FAA to accommodate, integrate, and evolve
UAS into the NAS. The first steps established
Section 333 Exceptions to accommodate UAS in the NAS, and recently Part 107
rules addressed the small UAS.
There exist manned
aircraft technologies that will assist in integrating the UAS to the NAS. However, these technologies may not apply for
some of the UAS, particularly the smaller airframes. Part 107 addresses some of these
shortcomings. One would expect that
future FAA rules will also accommodate larger UAVs, particularly in the 500 to
18,000 feet altitude range. Above 18,000 feet, the UAS will be required to
follow established FAA regulations.
References
AUVSI
Welcomes FAA Announcements at XPONENTIAL. (2016, May 05). Retrieved August 31,
2016, from http://www.auvsi.org/blogs/auvsi-advocacy/2016/05/05/xpofaaannouce
Clot,
A. (n.d.). Communications Command and Control: A Crowded Spectrum. Retrieved
August 31, 2016, from
http://ftp.rta.nato.int/public//PubFulltext/RTO/EN/RTO-EN-009///EN-009-02B.pdf
Clot,
A. (n.d.). Communications Command and Control: A Crowded Spectrum. Retrieved
August 31, 2016, from
http://ftp.rta.nato.int/public//PubFulltext/RTO/EN/RTO-EN-009///EN-009-02B.pdf
Operation
and Certification of Small Unmanned Aircraft Systems [PDF]. (2016, June
21). Washington, DC: Federal Aviation Administration.
Retrieved
from http://www.faa.gov/uas/media/RIN_2120-AJ60_Clean_Signed.pdf
Section
333. (n.d.). Retrieved August 31, 2016, from
https://www.faa.gov/uas/beyond_the_basics/section_333/
Section
333 vs. Part 107: What Works for You? (2016, August 29). Retrieved August 31,
2016, from http://www.faa.gov/news/updates/?newsid=86285
UAS
Integration. (2012, September 18). Retrieved August 31, 2016, from
https://www.youtube.com/watch?v=5eUyuK0u1fc. Interview: Chuck Johnson, Program
Manager for Unmanned Aircraft Systems Integration in the National Airspace
System at NASA Dryden Aircraft Operations Facility
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