| Literature DB >> 35632303 |
Wahab Khawaja1, Vasilii Semkin2, Naeem Iqbal Ratyal1, Qasim Yaqoob1, Jibran Gul1, Ismail Guvenc3.
Abstract
The use of unmanned aerial vehicles (UAVs) for different applications has increased tremendously during the past decade. The small size, high maneuverability, ability to fly at predetermined coordinates, simple construction, and affordable price have made UAVs a popular choice for diverse aerial applications. However, the small size and the ability to fly close to the terrain make the detection and tracking of UAVs challenging. Similarly, unmanned underwater vehicles (UUVs) have revolutionized underwater operations. UUVs can accomplish numerous tasks that were not possible with manned underwater vehicles. In this survey paper, we provide features and capabilities expected from current and future UAVs and UUVs, and review potential challenges and threats due to use of such UAVs/UUVs. We also overview the countermeasures against such threats, including approaches for the detection, tracking, and classification of UAVs and UUVs.Entities:
Keywords: classification; countermeasures; detection; tracking; unmanned aerial vehicles (UAVs); unmanned underwater vehicles (UUVs)
Mesh:
Year: 2022 PMID: 35632303 PMCID: PMC9143730 DOI: 10.3390/s22103896
Source DB: PubMed Journal: Sensors (Basel) ISSN: 1424-8220 Impact factor: 3.847
Popular categories of UAVs, major types of sensors installed, and their functionalities and features are provided. All the UAVs are equipped with GPS receivers, internal navigation unit(s), and control and data communication links.
| UAV Name | Category | Powered by and Sensors Installed | Functionalities | Maximum Payload, Speed, Flight Altitude and Duration |
|---|---|---|---|---|
| Malat Mosquito | Micro/nano, fixed-wing | Battery, camera, EO sensor | Surveillance and reconnaissance | 0.25 kg, 13 m/s, 0.15 km, 1 h |
| Aurora Skate | Micro/nano, fixed-wing | Articulating motor pods, camera, EO/IR sensors | Surveillance and reconnaissance, tracking objects | 0.2 kg, 25 m/s, 4.3 km, 1 h |
| CyberQuad mini | Micro/nano, multi-rotor | Battery, camera, and multiple sensors for detecting gases and pollutants | Urban aerial reconnaissance, detection of gases, industrial and other pollutants | 1.5 kg, 18 m/s, -, 0.67 h |
| RQ-11 Raven | Small/mini, fixed-wing | Battery, camera, infrared sensor, miscellaneous sensors | Surveillance, mapping, imaging and object detection and classification | 0.2 kg, 22.5 m/s, 4.2 km, 1.5 h |
| Matrice-600 | Small/mini, multi-rotor | Battery, camera, intelligent batteries | Imaging and surveillance, high data rate live streaming | 6 kg, 18 m/s, 2.5 km, 0.67 h |
| SkyEye Sierra VTOL | Small/mini, fixed-wing and multi-rotor | Battery/petrol engine, camera, surveying and surveillance equipment, multiple sensors | Imaging, mapping, inspection, and surveillance, and other sensing applications | 3 kg, 30 m/s, 3 km, 5 h |
| Watchkeeper | Medium, fixed-wing | Rotary Wankel engine, camera, EO/IR sensor, motion filter | Imaging, surveillance and reconnaissance | 150 kg, 40 m/s, 4.9 km, 14 h |
| Eagle Eye, Bell HV-911 | Medium, tiltrotor | Turboshaft engine, camera, surveillance sensors, rescue equipment | Search and rescue, surveillance, reconnaissance (mainly at sea) | 90 kg, 103 m/s, 6 km, 5.5 h |
| Skyeye-R4E | Medium, fixed-wing | Twin rotor rotary engine, camera, surveillance and miscellaneous sensors | Imaging, surveillance, pesticide spraying, border patrols | 82 kg, 55 m/s, 4.6 km, 8 h |
| Global Hawk | Large, fixed-wing | Turbofan engine, camera, EO/IR sensors, laser and radar warning receivers, ECM equipment, MTI system | Long endurance and high-altitude and wide area ground/sea surveillance and reconnaissance, communications | 1400 kg, 175 m/s, 18 km, 33 h |
| Zephyr 8 | Large, fixed-wing | Solar-powered, Amprius lithium-ion batteries, communication systems | Airborne communications: as a mobile communication relay | 5 kg, 9.5 m/s, 21.3 km, 26 days |
Figure 1The high-level design of a futuristic UAV. Multiple sensors and sources of energy can be used. In particular, variable wing geometry can be used during different modes of flight. The variable wing geometry can help to obtain different flight speeds and to make vertical take-off and landing possible.
Comparison of current and expected future UAV features and capabilities.
| Serial # | Current UAV Features and Capabilities | Future UAV Features and Capabilities |
|---|---|---|
| 1 | Multi-rotor or fixed-wing | Hybrid of multi-rotor and fixed-wing, variable wing geometry |
| 2 | Aerial flying | Aerial, over- and underwater, and on-ground maneuvering |
| 3 | Propeller propulsion | Jet engine propulsion in addition to propeller propulsion |
| 4 | Battery and fossil fuel | Solar, synthetic, hydrogen fuel, and battery charging while flying |
| 5 | Small and medium payloads | Large, multi-purpose payloads |
| 6 | Limited maneuverability for fixed-wing UAVs | High maneuverability for fixed-wing UAVs |
| 7 | Cost varies, and dependent on the size of UAV | Reduction in price of different sizes of UAVs |
| 8 | Flight duration dependent on the payload | Long flight duration, and less dependent on the payload |
| 9 | Weather and light affects performance | All weather, day and night high performance |
| 10 | Small to medium RCS | Very small RCS |
| 11 | Limited and vulnerable communication links | Redundant and secured communication links |
| 12 | Semi-autonomous operations | Fully autonomous and AI-controlled options available |
| 13 | Limited ECM capabilities | Enhanced ECM capabilities |
Figure 2Different types of radars for detection, identification, and tracking of aerial vehicles. Primary radars are used for detection of aerial objects, whereas secondary radars are used for identification. Primary radars are sub-categorized into continuous wave and pulse radar.
Figure 3Detection and tracking of multiple UAVs with the help of 60 GHz FMCW frequency-division multiplexing MIMO radar [57].
Figure 4A micro-Doppler simulation scenario using a monostatic radar and four-blade helicopter [90]. The monostatic radar is immovable and is placed at the origin. The initial helicopter coordinates are . The blades of the helicopter rotate at four revolutions per second, and the velocity of the helicopter is 80 m/s.
Figure 5The range-velocity plot of the setup is shown in Figure 4 (reprinted from [90]). The major power concentration is centered at ( m/s, 975 m) due to the central rotation part of the helicopter. The other two minor concentrations are due to the radar returns from the tips of the blades.
Figure 6Micro-Doppler modulation due to (1) rotating blades and (2) a constant Doppler shift from the central rotating part of the helicopter (reprinted from [90]). The sinusoidal behavior is due to the rotation of the blades.
Figure 7Setup for detection of a UAV using RF analysis. The RF link is between the ground controller and flight controller. Based on the energy detection of the RF link, a UAV can be detected and subsequently classified (reproduced from [97]).
Comparison of current and future research directions for countering malicious UAVs.
| Current Countermeasures Cgainst UAVs | Future Cirections of Countermeasures against UAVs |
|---|---|
|
Radars Acoustic analysis RF analysis EO/IR imaging RF jamming, remote hacking, and GPS spoofing High-power laser and EM radiation Nets and prey birds |
Modifications to current radar systems specifically for UAVs Mesh of laser beams Distributed sensors at different locations AI-aided cognitive analysis of the threat using multiple sensors Regulating legitimate UAV aerial traffic through tagging Use of satellite networks for UAV detection and tracking |
Figure 8Bi-static sensors placed at different locations are shown as inverted triangles for aerial vehicle detection (reprinted from [117]). Four ellipsoids indicate the coverage of the respective bi-static sensors. A single emitter is shown as a purple circle at the origin. The aerial vehicle is shown as a white diamond wrapped around by a yellow circle indicating fused detections. The fused detections due to the overlapping of the ellipsoids are close to the actual position of the aerial vehicle. The trajectory is shown as a grey line.
Figure 9A mesh of laser beams was created using two airborne UAVs (reprinted from [89]). Each airborne UAV produces a uniformly spaced array of laser beams. A mesh is formed by the appropriate positioning of the airborne UAVs. The laser mesh can be used to detect, track, and classify different types of targets [89].
Figure 10In addition to conventional layers for countering UAVs (layers 2 and 3), we have introduced layer 1 sensors. The first layer sensors are placed at different locations. The first layer can help in the early detection, tracking, and classification of intruding UAVs.
Popular UUVs, types of sensors installed, dimensions of the UUVs, and maximum endurance and depths underwater are provided. All the UUVs provided here are autonomous and are used for deepwater and seafloor imaging/mapping and oceanography research.
| Sr. # | UUAV Name | Powered by and Sensors Installed | Dimensions, Endurance and Depth |
|---|---|---|---|
| 1 | MBARI’s Dorado-class | Battery, 200 kHz multibeam sonar, 100 kHz and 410 kHz chirp sidescan sonars | 0.5 m diameter, 6.4 m length, 20 h endurance, 6 km depth |
| 2 | Sentry | Battery, conductivity, temperature and depth sensors, digital camera, reodx potential probe | 1.8 m height, 2.2 m width, 2.9 m length, 24 h endurance, 6 km depth |
| 3 | Qianlong-1 | Battery, camera, obstacle avoidance sonar, side-scan sonar | 0.8 m diameter, 4.6 m length, 24 h endurance, 6 km depth |
| 4 | SeaBED Class | Battery, Imagenex Delta-T imaging sonar, camera | 2 m length, 1.5 m height, 1.2 m width, 24 h endurance, depth 5 km |
| 5 | Urashima (hybrid) | Battery, multi-beam echo sounder, Niskin water sampler, interferometric synthetic aperture sonar, gravimeter system | 1.3 m width, 10 m length, 24 h endurance, depth 3.5 km |
| 6 | Aster x/Idef x | Battery, multi-beam echo sounders, multiple sensors, sub-bottom profilers, spectrometers | 0.7 m diameter, 4.5 m length, 16 h endurance, depth 3 km |
| 7 | BlueROV2 | Battery, gyroscope, accelerometer, magnetometer, pressure/depth and temperature sensor | 457 mm × 338 mm × 254 mm, 4.5 m, 4 h endurance, depth 300 m |
Figure 11Block diagram of signal processing for (a) active sonar, (b) passive sonar.
Different frequencies and applications of sonar.
| Serial # | Frequencies | Application |
|---|---|---|
| 1 | 3–30 Hz, ELF band | Underwater communications and pinging |
| 2 | 30–300 Hz, super low frequency (SLF) band | Underwater submarine communications |
| 3 | 300 Hz–3 kHz, ultra low frequency (ULF) band | Underwater communications through dirt and rocks |
| 4 | 3 kHz–30 kHz, very low frequency (VLF) band | Near-sea-surface communications, navigation beacons |
| 5 | 30 kHz–300 kHz, low frequency (LF) band | Near-sea-surface communications, navigation beacons |
| 6 | 3 kHz–30 kHz, VLF band | Near sea surface communications, navigation beacons |
| 7 | Less than 1 kHz, 1 kHz–10 kHz, greater than 10 kHz, and less than 30 kHz | Active sonar operation |
| 8 | 50 kHz, 120 kHz, 200 kHz, and 455 kHz | Sport fishing |
| 9 | 120 kHz, and 200 kHz | Sea floor imaging using deep towed sonar, and swath phase-bathymetric mapping |
| 10 | 100 kHz–1 MHz | Side-scan sonar |
Figure 12A towed active sonar carried by a surface ship for detection of a submerged UUV/MUV. The sonar is towed to avoid noise (sound) from the carried vessel.
Figure 13Sonar-based detection of a remotely operated underwater vehicle. Active sonar equipment is mounted on a remotely operated underwater vehicle. Detection is highlighted in yellow in the sonar scan.