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A novel airborne self organising architecture for 5G+ Networks
Shakir, Muhammad Zeeshan; Ahmadi, Hamed; Katzis, Konstantinos
Published in:
2017 IEEE 86th Vehicular Technology Conference (VTC Fall)
DOI:
10.1109/VTCFall.2017.8288095
Published: 12/02/2018
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Peer reviewed version
Link to publication on the UWS Academic Portal
Citation for published version (APA):
Shakir, M. Z., Ahmadi, H., & Katzis, K. (2018). A novel airborne self organising architecture for 5G+ Networks. In
2017 IEEE 86th Vehicular Technology Conference (VTC Fall) IEEE.
https://doi.org/10.1109/VTCFall.2017.8288095
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1
A Novel Airborne Self-organising Architecture for
5G+ Networks
Hamed Ahmadi, Senior Member, IEEE, Konstantinos Katzis, Senior Member, IEEE, and
Muhammad Zeeshan Shakir, Senior Member, IEEE
Abstract—Network Flying Platforms (NFPs) such as unmanned aerial vehicles, unmanned balloons or drones flying at
low/medium/high altitude can be employed to enhance network
coverage and capacity by deploying a swarm of flying platforms
that implement novel radio resource management techniques. In
this paper, we propose a novel layered architecture where NFPs,
of various types and flying at low/medium/high layers in a swarm
of flying platforms, are considered as an integrated part of the
future cellular networks to inject additional capacity and expand
the coverage for exceptional scenarios (sports events, concerts,
etc.) and hard-to-reach areas (rural or sparsely populated areas).
Successful roll-out of the proposed architecture depends on
several factors including, but are not limited to: network optimisation for NFP placement and association, safety operations
of NFP for network/equipment security, and reliability for NFP
transport and control/signaling mechanisms. In this work, we
formulate the optimum placement of NFP at a Lower Layer
(LL) by exploiting the airborne Self-organising Network (SON)
features. Our initial simulations show the NFP-LL can serve more
User Equipment (UE)s using this placement technique.
Index Terms—Airborne SON; 5G+ wireless networks; radio
access network (RAN); networked flying platforms (NFPs);
unmanned aerial vehicle (UAV); drones; low altitude platform
(LAP); medium altitude platform (MAP); high altitude platform
(HAP);
I. I NTRODUCTION
The Fifth Generation (5G) networks, which are expected to
be rolled out soon after 2020, will support a 1000 times higher
average data traffic, 10-100 fold increase in data rate and
connected devices [1]. One of the enabling solutions to meet
the demand for high data rate is the densification in cellular
network by complementing the ultra-dense deployment of low
power small base stations (SBSs) with the airborne cellular
network and forming a multi-tier heterogeneous network (HetNet) for 5G+ systems.
One of the biggest challenges in designing such an airborne
cellular network communication system, is to optimally position the flying Base Station (BS) or drone-cell and maintain that position so that the network can benefit the most.
Extensive work by numerous research groups investigated
how the position of the flying BS or drone-cell can affect
the performance of the aerial and terrestrial communication
systems as well how its position can play a vital role in the
operation of the network. For instance, in [2] authors looked
at the effect of different generic mobility models that can
be used to characterize the pertinent movements of HAPs
H. Ahmadi is with the School of Electrical and Electronic Engineering,
University College Dublin, Ireland, Email:
[email protected].
K. Katzis is with the Department of Computer Science and Engineering,
European University Cyprus, Cyprus, Email:
[email protected].
M. Z. Shakir is with the School of Engineering and Computing, University of the West of Scotland, Paisley, Scotland, UK, Email:
[email protected].
and their effect on the communications. Furthermore, system
operating parameters such as the flight path, operation location
and service duration over a particular service area can be of
high significance in terms of optimized communications for
the users on the ground if the aim is to provide seamless connectivity during handoff between platforms [3]. [4] introduces
a genetic Interference-aware Positioning of Aerial Relays
(IPAR) algorithm which is able to find suitable positions
for the UAVs that maximize the downlink throughput of the
cellular network. Similarly, [5] discusses efficient algorithms
developed to compute the optimal position of the drone for
maximizing the data rate, which are shown to be highly
effective via simulations. In [6], authors presents that the
optimal altitude is a function of the maximum allowed pathloss
and of the statistical parameters of the urban environment, as
defined by the International Telecommunication Union. They
also present a closed-form formula for predicting the probability of the geometrical line of sight between a Low Altitude
Platform (LAP) and a ground receiver. In [7] authors present a
3-D placement problem with the objective of maximizing the
revenue, which is measured by the maximum number of users
covered by the drone-cell. To solve this problem, they have
formulated an equivalent problem which was solved efficiently
to find the location and size of the coverage region, and the
altitude of the drone-cell.
An airbone cellular network comprises of Network Flying
Platform (NFP)s of various types including Unmanned Aerial
Vehicle (UAV)s, drones, balloons, and high-altitude/mediumaltitude/low-altitude platforms (HAPs/MAPs/LAPs) to expand
the cellular coverage and deliver Internet services to remote
and dedicated regions where infrastructure is not available
and expensive to deploy. However, a major challenge in such
networks is how to design and manage Self-organisation in
cellular networks which is mostly seen as a result of distributed
decision making [8]. In conventional SON, self-configuration,
self-optimization and self-healing are considered as main SON
functions. An airborne cellular network has a more dynamic
nature compared to a fixed cellular network because the
position of its elements may change over the time. This may
be due to change in demand, weather conditions, coverage
requirements, battery limitations and even due to some realtime traffic changes/abnormalities in the network. In such
an airborne cellular network each BS i.e., NFP-LL, must
be capable of performing a combination of conventional and
emerging SON functionalities for airborne cellular network
depending on the role of NFPs in the network.
The rest of the paper is organised as follows: A novel airborne cellular architecture is introduced in Section II. Section
III presents optimisation problem of the proposed airborne
SON and its implementation. Section IV presents simulation
2
Fig. 1. Graphical illustration of the hierarchical airborne self organizing architecture where variety of NFPs are flying at different altitudes and are offering
a complementary wireless network.
results and some discussions on the results. Conclusions
are drawn under section V and finally some challenges are
summarised in Section VI.
II. A IRBORNE S ELF O RGANISING N ETWORKS
In an emerging airborne cellular network, the SON functionalities can be realized differently. For example, when a
cell outage is detected, neighboring BSs in conveantional
SON compensate this outage by increasing their transmission
power or changing their antenna tilt (self-healing) while in
an airborne SON, NFPs can also effectively reorganise their
positions to compensate the outage with lower energy consumption. The new placements can be decided centrally or
locally at each NFP element – distributed decision making.
deployment are more prone to the associated network security
risks including their safe operation and security of information.
In our architecture, NFPs in the medium layer are dual role
playing i.e., in addition to relaying, medium altitude platforms
(MAPs) are performing surveillance to ensure safe and secure
operation of the architectures. The surveillance operation
includes network monitoring, surveillance scheduling, and
decisions to further optimise the network and ensure reliable
and secure operation by exploiting the collaboration between
the participating NFPs in the medium layer. NFPs in the lower
layer are optimally distributed to offer capacity and expand
coverage via resource and interference management. It is to
note that in the proposed architecture HAPs and MAPs are
flying with fixed/known locations, however, LAPs are flying
with relatively random or optimally distributed locations and
offering coverage or capacity in an optimal way.
A. Proposed Systems Architecture:
Fig. 1 shows our proposed novel layered architecture where
NFPs are distributed in a hierarchal manner such that the LL
is responsible for access or fronthaul for small cells, Higher
Layer (HL) is responsible for transport network and Medium
Layer (ML) is serving as a relay between the two layers.
NFPs in the LL are typical low altitude platforms (LAPs)
flying at relatively lower altitudes and responsible for network
optimisation including NPF placement and association based
on resource allocation, interference management, etc. On the
other side, NFPs such as UAV, unmanned balloons or drones
flying at low/high/medium altitude can be used to enhance
network coverage and capacity by deploying a swarm of flying
platforms that implement novel radio resource management
techniques [9]. In this paper, operating in the HL belong to
High Altitude Platform (HAP) category and are responsible
for optimising the resources in transport networks for lower
layers. NFPs in the ML belong to the Medium Altitude
Platform (MAP) category and are responsible for relaying the
network between the lower and higher layers in our proposed
architecture. Safety and security of the proposed NFPs driven
cellular network is of significant importance as such network
B. Functionalities of Layers in Proposed Architecture:
The general system architecture of our proposed NFP has
been divided into three layers of operation. The HL ranging
between 15km-25km, the ML ranging between 5km-15km and
the LL which is up to 5km height. For each layer, the operating
conditions can vary in terms of wind speed, humidity and
temperature. This means that certain type of platforms can
be operational at a particular layer, that can cope with the
flying conditions as well as provide their services which can
range from surveillance, broadband connectivity to backhaul
communications as described below.
1) HAP: is a stratospheric platform capable of delivering
a wide range of services such as mobile cellular communications, broadband wireless access as well as search and rescue
services. A HAP is expected to operate at the HL providing
Line of Sight (LOS) connectivity over a wide geographical
area (30km radius). Such platforms can either be planes or
airships, manned or unmanned that can carry a payload of a
few kilograms to a few tones and can stay airborne from a
few hours to a few years depending on their type, size, power
constraints and fuel capacity. A HAP can provide ubiquitous
3
TABLE I
S UMMARY OF AERIAL PLATFORMS PARTICIPAITING IN A IRBONE CELLULAR NETWORK .
Platform Name
AirShip
AirPlane
AirBaloon
AirCopter
(S/P/B/C)
Manned
Unmanned
Max Altitude
(approximately)
Platform
length
Platform width
(Wing Span)
Platform
weight
Range
Max
Payload
Endurance
(M/U)
(m)
(m)
(m)
(kg)
(km)
(kg)
(hrs)
25
2.7
16
2.26
0.5
40
1900
1.2
2343
100
380
25
0.5
0.37
Tethered
24
0.8
52
Tethered
6
9
34
7.1
10000
270
250
408
487
200
400
6
15
504
48
30
24
117
24
24
26
250
1700
1400
1360
2.27
99.79
250
7000
2700
52
14
8
32
30
24
5 years
6.5
10 years
Lower Layer - LAP
Amazon Drone
Aerovironment Dragon Eye
SkyHook (Helikites)
Zepellin-NT
MD4-1000 (DHL)
Skyship 600 (Charly)
Desert Star (Helikites)
MRI P2006T
Protonex
C
P
B
S
C
S
B
P
P
U
U
U
M
U
M
U
M
U
122
150
2286
2600
3000
3050
3352
4200
4250
0.9
7.31
75
1.03
59
10.05
8.7
1.1
5.48
19.5
1.03
15.2
6.7
11.4
8.2
Medium Layer - MAP
Schiebel Camcopter S-100
ScanEagle
Airlander 10
General Atomics Prowler II
FOTROS
EADS SDE Eagle 1
Solar Impulse 2
MQ-1 Predator
Anka - A
Silver Arrow Sniper
P
P
S
P
P
P
P
P
P
P
U
U
M
U
U
U
M
U
U
U
5486
5944
6100
7600
7600
7620
8534
8839
9144
9145
3.11
1.6
92
5
6.2
9.3
22.4
8.53
8
9.4
1.24
3.1
43
10.75
17
16.6
72
17
17.3
18
110
16
20000
250
Higher Layer - HAP
IAI Heron
Predator B (MQ-9B)
G520 Strto 1
Northrop Grumman Global Hawk
Zephyr 6
Aurora Flight Sciences Perseus
Stratobus
M-55 Geophysica
ISIS (Integrated Sensor is Structure)
P
P
P
P
P
P
S
P
S
U
U
M
U
U
U
U
M
U
10000
15000
16000
18000
18288
19812
20000
21000
21500
8.5
11
13.82
14.5
16.6
20
33
39.9
18
21.79
30
37.46
900
2223
3300
6781
30
1936
350
1852
3670
22779
13995
4965
coverage providing backhaul and control/fleet coordination
services for other aerial platforms at lower layers. A fleet
of HAPs can be used to provide extended communication
coverage and redundancy if necessary, while inter-platform
communications can be established employing Free Space
Optics (FSO).
2) MAP: are aerial platforms operating at the ML that can
be used as a relay between a HAP and a LAP. Depending on
the operation scenario, current available MAP in the market
are mostly UAV with long endurance capabilities as well as
manned aerial vehicles. UAV platforms can stay airborne for
several hours and are usually destined for military missions.
MAP coverage area is expected to be of up to 5km radius.
3) LAP: such as tethered balloons, drones, operate at the
LL. Like HAP and MAP, LAP exhibit common features
such as LOS communications with favorable radio conditions,
while they have the ability to rapidly deploy a fleet of LAP
with modular communication payload capabilities. LAP are
currently in high demand for public usage and the current
market is driving the drone industry in delivering newer and
smarter platforms, with higher endurance and greater range,
more agile and efficient aerial vehicles. LAP are optimally
distributed to offer capacity and expand coverage via resource
and interference management.
Table 1 lists a number of aerial platforms that can be
employed to carry out a mission on a particular layer. In LL,
LAP are expected to feature a relatively small size, limited
payload and endurance capabilities in minutes or hours while
offering rapid deployment operating below 5km height. LAP
are expected to operate in organised / scheduled shifts in order
to ensure continuity of service. MAP are expected to be able
7.62
100
22.86
137.16
8790
2.9
3757
850
50
1000
2300
1233
1400
1250
Fixed
900
20
1019
Fixed
926
600
180
2000
2000
1000
400
4896
200
to cope with a heavier payload in order to maintain their
role as network relays between LL and ML featuring more
functionalities than LAP. They are capable of staying aloft for
a greater duration of time (hours / days) in order to support the
operation of LAP. MAP are expect to be operational between
5-15km height subject to the local aviation regulations of
operation. Finally, HAP operating on HL will be of much
bigger size operating at a height around 17-20km height. Such
platforms will be carrying a much heavier payload that would
support Radio Frequency (RF) and FSO communications. It
should be able to stay operational for days/months without
require refueling. A possible scenario is to use Protonex as
LAP that can stay aloft up to 9 hours while the Airlander10
can operate as MAP providing services at about 10km height.
Finally, a HAP such as ISIS can stay aloft for a great duration
of time providing connectivity to the MAP.
III. O PTIMISATION OF A IRBONE SON
In our proposed architecture the position of LAPs in the LL
is defined centrally and the NFP has the ability to re-organise
the LL to achieve its target, which can be capturing as many
UEs, maximizing the achievable rate, and/or fairness among
UEs. However, optimum placement is an NP-hard problem.
NFP-LL placement to capture maximum UEs can be for-
4
of the global solution. Compared to GA and ACO modeling
the mixed integer problems is more straightforward in PSO.
mulated as:
max
U
N X
X
n=1 u=1
U
X
dn,u
B. Decentralized decision making:
In the proposed architecture we use centralized decision
making
to define the position of LAP in LL. However, the
u=1
architecture has the potential to integrate a distributed decision
1 RSSn,u > RSS−n,u
dn,u =
∀u ∈ {1, . . . , U }, making mechanism for positioning the LAP. Game theory is
0
otherwise
the most popular techniques used for designing and analyzing
where N is the number of LAPs in NFP-LL, U is the number distributed decision making approaches [15]. Different classes
of UEs, and dn,u is 1 if the uth UE is served by LAP of game theoretic approaches can be used to model compen, otherwise it will be zero. RSSn,u denotes the received tition, cooperation, and coalition between different players,
signal strength of UE u from LAP n. RSS−n,u denotes the LAPs. Game theoretic analysis of the system tells that if
strengths of received signal from other nodes of NFP and the there exists a path that leads the competition/cooperation of
independent decision makers to an equilibrium. In other words,
Macrocells, if exists.
The above mixed integer nonlinear problem can be lin- it enables the system designers to avoid objective functions
earized using the technique presented in [10] and commercial that lead the system to instability.
In an airborne network settings, parameters of the network
packages like CPLEX can solve the mixed integer linear
problem. Problems with limited number of UEs, and LAPs will change much faster than a terrestrial network. Therefore,
serving as hotspots can be solved with exhaustive search. In learning from past experiences is extremely important in both
this work we use this technique. However, in more complex centralized and decentralized decision making mechanisms
scenarios even the mixed integer linear problem will be too for airborne SON [16]. In decentralized systems, learning
complex. Therefore, metaheuristic algorithms can be used to techniques help reaching an equilibrium in fewer iterations.
find an efficient sub-optimum solution [11]. We introduce
some of these metaheuristic methods.
subject to
dn,u ≤ 1,
∀n ∈ {1, . . . , N }
70
Airborne SON
Fixed placement
60
Number of captured UEs
A. Resource allocation using metaheuristics:
Popular metaheuristics in radio resource allocation are Genetic Algorithms (GA), Ant Colony Optimization (ACO), and
Particle Swarm Optimization (PSO).
1) GA: code the solution into a chromosome (also known
as individual) and evaluates the optimality of the solution
with a function called fitness function [12]. In this work the
fitness function is the sum captured UEs, and the chromosome
consists of the position of UAVs. Crossover and mutation are
tools of GA for improving the solutions. Crossover combines
fragments of two chromosomes and creates a new chromosome
which is another solution in the feasible area. Mutation is
the tool which is hired for overcoming the local optimums;
mutation changes a gene randomly with the hope of reaching better solutions. The algorithm starts with a randomly
generated population of chromosomes and at each iteration it
creates a generation of offspring using crossover and mutation.
The fittest of parent and offspring generations are kept for
the next iteration and the rest are discarded. This way GA
keep the population size constant. The algorithm stops after
the maximum number of iterations is reached.
2) ACO: has been used in radio resource management for
network planning and spectrum allocation [13]. The main idea
is taken from the way ants find the shortest path to the food
using pheromone. The shorter and more popular paths have
higher density of pheromone while longer paths will lose
pheromone due to the evaporation. In this model each solution
will be coded as a path, and at each iteration each ant chooses
a path with a probability that is proportional to the amount
of pheromone. After a certain number of iterations the most
popular will be selected, i.e. the algorithm converges.
3) PSO: models the social behavior of a group of birds
[14]. It consists of a swarm of candidate solutions called
particles, which explore an n-dimensional hyperspace in search
50
40
30
20
10
0
1
2
3
4
number of LAPs serving the hotspot
Fig. 2. Number of UEs captured by airborne SON compared to the fixed
placement of LAPs in NFP-LL. The network has 150 UEs where a third of
them are in the demand hotspot. Demand hotspot has a radius of 250 m (e.g.
outdoor concert area).
IV. S IMULATION RESULTS AND DISCUSSIONS
We modeled an NFP where the LL provides service to a
demand hotspot. The UEs in the system are served by the
macrocell and the NFP-LL assists the macrocell by capturing
UEs. The NFP optimizes its LL for a given number of LAPs.
Due to weather conditions, battery failure or surveillance duty
the system may lose an LAP. In this work, we compared
an airborne SON system that reorganizes itself with an NFP
with fixed LL placement. Our results in Fig. 2 shows that
the airborne SON outperforms the fixed placement. Crosslayer optimisation approaches are required to optimise the
placement or positioning of NFPs across the layers in proposed
airborne SON.
5
V. C HALLENGES AND FUTURE DIRECTIONS
Although airborne systems have attracted industry and
academia’s attention in the last couple of years, there still exists several challenges and open research directions. Following
are some of the important challenges for future airborne SON:
A. Standardization
Airborne cellular networks are yet to be standardized. The
existing networking standards cannot fully address the challenges of airborne networks and proper standards for airborne
communication and networking is required.
B. Surveillance
Airborne cellular network would offer complementary connectivity services to expand the coverage or inject the capacity
under some unknown situations, therefore their successful
operation would depend on advanced surveillance mechanisms
to detect amateur flying platforms and combat to avoid any
further disruption in cellular services.
C. Information security
Secure transmission of information over wireless links is
still a challenge for future Internet architecture. In our proposed system, NFPs in all layers have the ability to move
and complement the existing network, therefore, the dynamic
nature of the airborne cellular network could be an additional
challenge to ensure secure coverage expansion or capacity
enhancement.
D. Ethics and privacy
NFPs and swarm of NFPs may face two-fold challenges
in order to comply with regulatory issues related to privacy
and ethics. NFPs should be able to protect the privacy of
the connected users while following the flying ethics as per
regulations and avoiding no-flying zone.
E. Testbed and verification
Various projects in Europe and United States study and
test the performance of future Internet and connectivity architecture, resource allocation techniques, waveforms, and
integration of future technologies using advanced testbeds
[17]. To the best of our knowledge, none of the existing testbed
validation and experimentation provide an environment for
testing the proposed airborne SON.
VI. C ONCLUSIONS
In this paper we have presented a novel layered architecture
where NFPs, of various types and flying in low/medium/high
layers in a swarm of flying platforms, are considered as
an integrated part of the future cellular networks to inject
additional capacity and expand the coverage for exceptional
scenarios and hard-to-reach areas. In our proposed architecture
the position of LAPs in the LL is defined centrally and the
NFP has the ability to re-organise the LL to achieve its
target, which can be capturing as many UEs, maximizing the
achievable rate, and/or fairness among UEs. To evaluate the
proposed architecture, we compared an airborne SON system
that reorganizes itself with an NFP with fixed LL placement.
Our results show that the airborne SON outperforms the fixed
placement.
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