On the Use of Unmanned Aerial Systems for Environmental Monitoring
Abstract
:1. Introduction
2. Data Collection, Processing, and Limitations
2.1. Preflight Planning
2.2. Sensors
2.3. Software
3. Monitoring Agricultural and Natural Ecosystems
3.1. Vegetation Monitoring and Precision Agriculture
3.2. Monitoring of Natural Ecosystems
4. River Systems and Floods
Flow Monitoring
5. Final Remarks and Challenges
- (i)
- While a direct comparison between different methodologies (UAS, manned airborne, and satellite) is challenging, it was found that UAS systems represent a cost-effective monitoring technique over small regions (<20 ha). For larger extents, manned airborne or satellite platforms may become more effective options, but only when the temporal advantage of the UAS is not considered.
- (ii)
- The limited extent of the studied areas reduces the relative budget available, increasing the fragmentation of the adopted procedures and methodologies.
- (iii)
- Government regulations restricting the Ground Sample Distance (GSD) and the UAS flight mode are limiting the economic advantages related to their use and some potential applications, particularly in urban environments.
- (iv)
- The wide range of experiences described highlighted the huge variability in the strategies, methodologies, and sensors adopted for each specific environmental variable monitored. This identifies the need to find unifying principles in UAS-based studies.
- (v)
- Vulnerability of UAS to weather conditions (e.g., wind, rain) can alter quality of the surveys.
- (vi)
- There are also technical limits, such as weather constraints (strong wind and/or rain), high elevations, or high-temperature environments that can be challenging for most of the devices/sensors and respective UAS operators (see, e.g., [155]).
- (vii)
- The geometric and radiometric limitations of current lightweight sensors make the use of this technology challenging.
- (viii)
- The high spatial resolution of UAS data generates high demand on data storage and processing capacity.
- (ix)
- There is a clear need for procedures to characterize and correct the sensor errors that can propagate in the subsequent mosaicking and related data processing.
- (x)
- Finally, a disadvantage in the use of UAS is represented by the complexity associated to their use that is comparable to that of satellites. In fact, satellite applications are generally associated to a chain of processing assuring the final quality of data. In the case of UAS, all this is left to the final user or researcher, requiring additional steps in order to be able to use the retrieved data.
- One of the aspects directly impacting the area that is able to be sensed is the limited flight times of UAS. This problem is currently managed by mission planning that enables management of multiple flights. Technology is also offering new solutions that will extend the flight endurance up to several hours, making the use of UAS more competitive. For instance, new developments in batteries suggest that the relatively short flying time imposed by current capacity will be significantly improved in the future [156]. In this context, another innovation introduced in the most recent vehicles is an integrated energy supply system connected with onboard solar panels that allow flight endurance to be extended from 40–50 min up to 5 h, depending on the platform.
- The relative ground sampling distance affects the quality of the surveys, but is often not compensated for. This limitation can now be solved by implementing 3D flight paths that follow the surface in order to maintain a uniform GSD. Currently, only a few software suites (e.g., UgCS, eMotion 3) use digital terrain models to adjust the height path of the mission in order to maintain consistent GSD.
- The influence of GSD may be reduced by increasing flight height, making UAS even more cost-competitive (by increasing sensed areas), but current legislation in many jurisdictions limits this to between 120 and 150 m and to within visible line of sight (VLOS). In this context, the development of microdrones will significantly reduce risk associated with their use, and relax some of the constraints due to safety requirements.
- Recent and rapid developments in sensor miniaturization, standardization, and cost reduction have opened new possibilities for UAS applications. However, limits remain, especially for commercial readymade platforms that are used the most among the scientific community.
- Sensor calibration remains an issue, especially for hyperspectral sensors. For example, vegetation can be measured in its state and distribution using RGB, multispectral, hyperspectral, and thermal cameras, as well as with LiDAR.
- Image registration, correction, and calibration remain major challenges. The vulnerability of UAS to weather conditions (wind, rain) and the geometric and radiometric limitations of current lightweight sensors have stimulated the development of new algorithms for image mosaicking and correction. In this context, the development of open source and commercial SfM software allows image mosaicking to be addressed, but radiometric correction and calibration is still an open question that may find a potential solution through experience with EO. Moreover, the development of new mapping-quality cameras has already significantly improved spatial registration and will likely help to also improve the overall quality of the UAS imagery.
Acknowledgments
Author Contributions
Conflicts of Interest
Appendix A. Available Sensors and Cameras
Manufacturer and Model | Sensor Type Resolution (MPx) | FormatType * | Sensor Size (mm2) | Pixel Pitch (μm) | Weight (kg) | Frame Rate (fps) | Max Shutter Speed (s−1) | Approx. Price ($) |
---|---|---|---|---|---|---|---|---|
Canon EOS 5DS | CMOS 51 | FF | 36.0 × 24.0 | 4.1 | 0.930 | 5.0 | 8000 | 3400 |
Sony Alpha 7R II | CMOS 42 | FF MILC | 35.9 × 24.0 | 4.5 | 0.625 | 5.0 | 8000 | 3200 |
Pentax 645D | CCD 40 | FF | 44.0 × 33.0 | 6.1 | 1.480 | 1.1 | 4000 | 3400 |
Nikon D750 | CMOS 24 | FF | 35.9 × 24.0 | 6.0 | 0.750 | 6.5 | 4000 | 2000 |
Nikon D7200 | CMOS 24 | SF | 23.5 × 15.6 | 3.9 | 0.675 | 6.0 | 8000 | 1100 |
Sony Alpha a6300 | CMOS 24 | SF MILC | 23.5 × 15.6 | 3.9 | 0.404 | 11.0 | 4000 | 1000 |
Pentax K-3 II | CMOS 24 | SF | 23.5 × 15.6 | 3.9 | 0.800 | 8.3 | 8000 | 800 |
Foxtech Map-01 | CMOS 24 | APS-C | 23.5 × 15.6 | 3.9 | 0.155 | 6 | 4000 | 880 |
Canon EOS 7D Mark II | CMOS 20 | SF | 22.3 × 14.9 | 4.1 | 0.910 | 10.0 | 8000 | 1500 |
Panasonic Lumix DMC GX8 | CMOS 20 | SF MILC | 17.3 × 13.0 | 3.3 | 0.487 | 10.0 | 8000 | 1000 |
Sony QX1 | CMOS 20 | APS-C | 23.2 × 15.4 | 4.3 | 0.216 | 3.5 | 4000 | 500 |
Ricoh GXR A16 | CMOS 16 | SF | 23.6 × 15.7 | 4.8 | 0.550 | 2.5 | 3200 | 650 |
Manufacturer and Model | Resolution (Mpx) | Size (mm) | Pixel Size (μm) | Weight (kg) | Number of Spectral Bands | Spectral Range (nm) | Approx. Price ($) |
---|---|---|---|---|---|---|---|
Tetracam MCAW6 (Global shutter) | 1.3 | - | 4.8 × 4.8 | 0.55 | 6 | 450–1000 (*) | 16,995 |
Tetracam MCAW12 (Global shutter) | 1.3 | - | 4.8 × 4.8 | 0.6 | 12 | 450–1000 (*) | 34,000 |
Tetracam MicroMCA4 Snap (Global shutter) | 1.3 | 115.6 × 80.3 × 68.1 | 4.8 × 4.8 | 0.497 | 4 | 450–1000 (*) | 9995 |
Tetracam MicroMCA6 Snap (Global shutter) | 1.3 | 115.6 × 80.3 × 68.1 | 4.8 × 4.8 | 0.53 | 6 | 450–1000 (*) | 14,995 |
Tetracam MicroMCA12 Snap (Global shutter) | 1.3 | 115.6 × 155 × 68.1 | 4.8 × 4.8 | 1 | 12 | 450–1000 (*) | 29,995 |
Tetracam MicroMCA6 RS (Rolling shutter) | 1.3 | 115.6 × 80.3 × 68.1 | 4.8 × 4.8 | 0.53 | 6 | 450–1000 (*) | 12,995 |
Tetracam MicroMCA12 RS (Rolling shutter) | 1.3 | 115.6 × 155 × 68.1 | 4.8 × 4.8 | 1 | 12 | 450–1000 (*) | 25,995 |
Tetracam ADC micro | 3.2 | 75 × 59 × 33 | 3.2 × 3.2 | 0.9 | 6 | 520–920 (Equiv. to Landsat TM2, 3, 4) | 2995 |
Quest Innovations Condor-5 ICX 285 | 7 | 150 × 130 × 177 | 6.45 × 6.45 | 1.4 | 5 | 400–1000 | - |
Parrot Sequoia | 1.2 | 59 × 41 × 28 | 3.75 × 3.75 | 0.72 | 4 | 550–810 | 5300 |
MicaSense RedEdge | 120 × 66 × 46 | 0.18 | 5 | 475–840 | 4900 | ||
Sentera Quad | 1.2 | 76 × 62 × 48 | 3.75 × 3.75 | 0.170 | 4 | 400–825 | 8500 |
Sentera High Precision NDVI and NDRE | 1.2 | 25.4 × 33.8 × 37.3 | 3.75 × 3.75 | 0.030 | 2 | 525–890 | - |
Sentera Multispectral Double 4K | 12.3 | 59 × 41 × 44.5 | - | 0.080 | 5 | 386–860 | 5000 |
SLANTRANGE 3P NDVI | 3 | 146 × 69 × 57 | - | 0.350 | 4 | 410–950 | 4500 |
Mappir Survey2 | 16 | 59 × 41 × 30 | 1.34 × 1.34 | 0.047 | 1–6 (filters)—one lens | 395–945 | 280 |
Mappir Survey3 | 12 | 59 × 41.5 × 36 | 1.55 × 1.55 | 0.050 | 1–4 (filters)—one lens | 395–945 | 400 |
Mappir Kernel | 14.4 | 34 × 34 × 40 | 1.4 × 1.4 | 0.045 | 19+ (filters)—six array lens | 395–945 | 1299 |
Manufacturer and Model | Lens | Size (mm2) | Pixel Size (μm) | Weight (kg) | Spectral Range (nm) | Spectral Bands (N) (Resolution, nm) | Peak SNR | Approx. Price ($) |
---|---|---|---|---|---|---|---|---|
Rikola Ltd. hyperspectral camera | CMOS | 5.6 × 5.6 | 5.5 | 0.6 | 500–900 | 40 (10 nm) | - | 40,000 |
Headwall Photonics Micro-hyperspec X-series NIR | InGaAs | 9.6 × 9.6 | 30 | 1.025 | 900–1700 | 62 (12.9 nm) | - | - |
BaySpec’s OCI-UAV-1000 | C-mount | 10 × 10 × 10 | N/A | 0.272 | 600–1000 | 100 (5 nm)/20–12 (15 nm) | - | - |
HySpex Mjolnir V-1240 | - | 25 × 17.5 × 17 | 0.27 mrad | 4.0 | 400–1000 | 200 (3 nm) | >180 | - |
HySpex Mjolnir S-620 | - | 25.4 × 17.5 × 17 | 0.54 mrad | 4.5 | 970–2500 | 300 (5.1 nm) | >900 | - |
Specim-AISA KESTREL16 | push-broom | 99 × 215 × 240 | 2.3 | 600–1640 | Up to 350 (3–8 nm) | 400–600 | - | |
Cornirg microHSI 410 SHARK | CCD/CMOS | 136 × 87 × 70.35 | 11.7 μm | 0.68 | 400–1000 | 300 (2 nm) | - | - |
Resonon Pika L | 10.0 × 12.5 × 5.3 | 5.86 | 0.6 | 400–1000 | 281 (2.1 nm) | 368–520 | - | |
CUBERT (S185) | Snapshot + PAN | 19 × 42 × 65 | 0.49 | 450–995 | 125 (8 mm) | - | 50,000 |
Manufacturer and Model | Resolution (Px) | Sensor Size (mm2) | Pixel Pitch (μm) | Weight (kg) | Spectral Range (μm) | Thermal Sensitivity (mK) | Approx. Price ($) |
---|---|---|---|---|---|---|---|
FLIR Duo Pro 640 | 640 × 512 | 10.8 × 8.7 | 17 | <0.115 | 7.5–13.5 | 50 | 10,500 |
FLIR Duo Pro 336 | 336 × 256 | 5.7 × 4.4 | 17 | <0.115 | 7.5–13.5 | 50 | 7500 |
FLIR Duo R | 160 × 120 | - | - | 0.084 | 7.5–13.5 | 50 | 2200 |
FLIR Tau2 640 | 640 × 512 | N/A | 17 | <0.112 | 7.5–13.5 | 50 | 9000 |
FLIR Tau2 336 | 336 × 256 | N/A | 17 | <0.112 | 7.5–13.5 | 50 | 4000 |
Optris PI 450 | 382 × 288 | - | - | 0.320 | 7.5–13 | 130 | 7000 |
Optris PI 640 | 640 × 480 | - | - | 0.320 | 7.5–13 | 130 | 9700 |
Thermoteknix Miricle 307 K | 640 × 480 | 16.0 × 12.0 | 25 | <0.170 | 8.0–12.0 | 50 | - |
Thermoteknix Miricle 110 K | 384 × 288 | 9.6 × 7.2 | 25 | <0.170 | 8.0–12.0 | 50/70 | - |
Workswell WIRIS 640 | 640 × 512 | 16.0 × 12.8 | 25 | <0.400 | 7.5–13.5 | 30/50 | - |
Workswell WIRIS 336 | 336 × 256 | 8.4 × 6.4 | 25 | <0.400 | 7.5–13.5 | 30/50 | - |
YUNCGOETEU | 160 × 120 | 81 × 108 × 138 | 12 | 0.278 | 8.0–14.0 | <50 | - |
Manufacturer and Model | Scanning Pattern | Range (m) | Weight (kg) | Angular Res. (deg) | FOV (deg) | Laser Class and λ (nm) | Frequency (kp/s) | Aprox. Price ($) |
---|---|---|---|---|---|---|---|---|
ibeo Automotive Systems IBEO LUX | 4 Scanning parallel lines | 200 | 1 | (H) 0.125 (V) 0.8 | (H) 110 (V) 3.2 | Class A 905 | 22 | - |
Velodyne HDL-32E | 32 Laser/detector pairs | 100 | 2 | (H)–(V) 1.33 | (H) 360 (V) 41 | Class A 905 | 700 | - |
RIEGL VQ-820-GU | 1 Scanning line | >1000 | 25.5 | (H) 0.01 (V) N/A | (H) 60 (V) N/A | Class 3B 532 | 200 | - |
Hokuyo UTM-30LX-EW | 1080 distances in a plane | 30 | 0.37 | (H) 0.25 (V) N/A | (H) 270 (V) N/A | Class 1905 | 200 | - |
Velodyne Puck Hi-Res | Dual Returns | 100 | 0.590 | (H)–(V) 0.1–0.4 | (H) 360 (V) 20 | Class A-903 | - | - |
RIEGL VUX-1UAV | Parallel scan lines | 150 | 3.5 | 0.001° | 330 | Class A-NIR | 200 | >120,000 |
Routescene—UAV LidarPod | 32 Laser/detector pairs | 100 | 1.3 | (H)–(V) 1.33 | (H) 360 (V) 41 | Class A-905 | - | - |
Quanergy M8-1 | 8 laser/detector pairs | 150 | 0.9 | 0.03–0.2° | (H) 360 (V) 20 | Class A-905 | - | - |
Phoenix Scout | Dual Returns | 120 | 1.65 | - | (H) 360 (V) 15 | Class 1-905 | 300 | >66,000 |
Phoenix ALS-32 | 32 Laser/detector pairs | 120 | 2.4 | - | (H) 360 (V) 10–30 | Class 1-905 | 700 | >120,500 |
YellowScan Surveyor | Dual returns | 100 | 1.6 | 0.125 | 360 | Class 1-905 | 300 | >93,000 |
YellowScan Vx | Parallel scan lines | 100 | 2.5–3 | - | 360 | Class 1-905 | 100 | >93,000 |
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Manfreda, S.; McCabe, M.F.; Miller, P.E.; Lucas, R.; Pajuelo Madrigal, V.; Mallinis, G.; Ben Dor, E.; Helman, D.; Estes, L.; Ciraolo, G.; et al. On the Use of Unmanned Aerial Systems for Environmental Monitoring. Remote Sens. 2018, 10, 641. https://doi.org/10.3390/rs10040641
Manfreda S, McCabe MF, Miller PE, Lucas R, Pajuelo Madrigal V, Mallinis G, Ben Dor E, Helman D, Estes L, Ciraolo G, et al. On the Use of Unmanned Aerial Systems for Environmental Monitoring. Remote Sensing. 2018; 10(4):641. https://doi.org/10.3390/rs10040641
Chicago/Turabian StyleManfreda, Salvatore, Matthew F. McCabe, Pauline E. Miller, Richard Lucas, Victor Pajuelo Madrigal, Giorgos Mallinis, Eyal Ben Dor, David Helman, Lyndon Estes, Giuseppe Ciraolo, and et al. 2018. "On the Use of Unmanned Aerial Systems for Environmental Monitoring" Remote Sensing 10, no. 4: 641. https://doi.org/10.3390/rs10040641