Page 159 - ITU Journal Future and evolving technologies – Volume 2 (2021), Issue 2

ITU Journal on Future and Evolving Technologies, Volume 2 (2021), Issue 2

Table 1 – Training data of 3D shape, maximum velocity, pitch and drift angles, and maximum altitude of targets and their respective categorization based
on shape.

Small Large Rockets
Multi‑ Fixed‑
Given Heli‑ ixed‑ ixed‑ Fighter Cruise Ballistic and
Target Type rotor wing Birds HGVs
target copters wing wing jets missiles missiles artillery
UAVs UAVs
planes planes shells
Category cat. 3 cat. 1 cat. 2 cat. 3 cat. 3 cat. 3 cat. 3 cat. 3 cat. 3 cat. 4 cat. 4 cat. 4
= = = = = = = = = = = =
Length (m) 5.65, = 1.94, = 21.4, = 7.8, = 13.63, = 56.8, = 20.26, = 6.48, = 0.69, = 14.1, = 3.3, = 5.3, =
0.05 1.3 16.2 6.15 9.3 14.6 6.2 2.6 0.4 11.1 2.5 4.5
= = = = = = = = = = =
Central part Width (m) 0.52, = 2.15, = 21.4, = 0.73, = 2.17, = 4.4, = 3.36, = 0.7, = NA 1.54, = 0.33, = 0.75, =
0.03 1.6 16.2 0.5 1.04 1.32 1.1 0.2 0.91 0.09 0.2
= = = = = = = = = = =
Height (m) 0.52, = 0.6, = 5.35, = 2.1, = 3.5, = 14.6, = 4.5, = 0.7, = NA 1.5, = 0.23, = 0.75, =
0.03 0.36 2.26 1.89 1.28 5.9 1.5 0.2 0.91 0.21 0.2
= = = = = = = =
Wing span 2.67, = NA 21.35, = 20.7, = 15.2, = 59.4, = 12, = 2.5, = 1.4, = NA NA NA
(m)
0.04 13.99 17.36 7.9 17.4 4.44 0.52 0.7
= = = = = = =
Wing 0.75, = NA NA 1.03, = 1.93, = 7.15, = 3.7, = 0.8, = 0.8, = NA NA NA
Wings and tail width (m) 0.02 0.62 0.94 2.36 1 0.4 0.5
sections span = = = = = = = =
and width Tail span 0.89, = NA 3.1, = 6.56, = 4.7, = 22, = 4.6, = 0.9, = 0.41, = NA NA NA
(m)
0.035 1.2 5.5 2.8 8 2.02 0.2 0.2
= = = = = = = =
Tail width 0.27, = NA 1, = 1.85, = 1.9, = 8.33, = 1.87, = 0.3, = 0.18, = NA NA NA
(m)
0.022 0.7 1.6 2.2 5.5 0.9 0.15 0.12
= = = = = = = = = = = =
(max) (m/s) 350.2, = 20.2, = 65.9, = 76.8, = 154.5, = 266.5, = 636, = 800, = 32.2, = 3500, = 937.5, = 4000, =
7.5 8.5 28.14 62.3 87 17.8 99.2 750 29.5 3000 593 2500
= = = = = = = = = = = =
∘ 12, = 10, = 15, = 20, = 10, = 8, = 20, = 12, = 10, = 5, = 5, = 10, =
8 5 25 30 20 15 45 30 30 30 15 60
= = = = = = = = = =
= =
∘ 15, = 10, = 15, = 8, = 7, = 15, = 8, = 5, = 5, = 8, =
7, = 5 5, = 8
10 15 20 15 15 40 10 15 20 45
= = = = = = = = = = = =
G
ℎ (km) 30, = 4.62, = 4.7, = 11.5, = 9.95, = 14, = 17.2, = 20, = 2.8, = 721, = 13.2, = 23, =
25 2.21 1.9 6.9 5.31 1.15 1.3 17.5 2 829 14.63 10.5
Table 2 – Size, velocity, and lying altitude of popular rotary and ixed‑wing UAVs.
Target Type Type Total area (max) (m/s) Max. altitude (km)
Length of central part (m) Wing span (m) Height of central part (m)
Phantom 4 [22] Multi‑rotor UAV 0.4 0.15, propellers dia 0.19 20 0.5
Matrice 600 [23] Multi‑rotor UAV 1.18 0.5, propellers dia 0.5 18 2.5
Amazon Prime Air [24] Multi‑rotor UAV 9.1 2.5, frame and propellers 1.5 22.2 0.15
MQ‑8B [25]] Helicopter UAV 7.3 8.4, propellers dia 2.9 59.2 6.1
Sky Surfer [26] Fixed‑wing UAV 0.91 1.4 0.32 13.8 0.2
Eclipse 2.0 [27] Fixed‑wing UAV 1.1 5.5 0.25 28 0.13
MQ‑9A [28] Fixed‑wing UAV 11 20 3.6 123.5 15.24
Global Hawk [29] Fixed‑wing UAV 14.5 35.4 4.7 175 19.8

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