Unmanned Aerial Systems (UAS) Research Laboratory


Unmanned Aerial Systems (UAS) Research Laboratory
Overview
The Unmanned Aerial Systems (UAS) Research Laboratory is focused on the design, engineering, and implementation of multimodal imaging systems, calibration techniques, and processing algorithms to provide the highest quality data with which to solve problems in the fields of precision agriculture, infrastructure inspection, and wildlife management.
Imaging Payloads
An Unmanned Aerial System (UAS) payload that features a cooled Hyperspectral SWIR that covers the ranges from 900-2500nm.
GPS/IMU: Applanix APX15
Accuracy Specifications | |
Position | 2-5 cm |
Velocity | .015 m/s |
Roll & Pitch | 0.25° |
True Heading | .08° |
MX-1 is a revolutionary new multi-modal remote sensing UAV payload that allows for simultaneous collection of four different imaging modalities namely RGB, LWIR, LiDAR and hyperspectral. MX1 is flown using a DJI Matrice 600 Pro UAV which has a weight of 10 kg, can carry a payload of 5.5 kg, and has a maximum controllable range of 5 km. The MX1 payload consists of the following sensors and specs at 30m altitude:
Modality | Sensor | # Bands | Spatial [px] | GSD [cm] |
---|---|---|---|---|
Hyperspectral | Headwall Nano-Hyperspec | 270 | 640 x 1 * | 1.88 |
RGB | Allied Vision Mako G-419 | 3 | 2048 x 2048 | 1.04 |
LWIR | DRS Tamarisk 640 | 1 | 640 x 480 | 3.09 |
LiDAR | Velodyne VLP-16 | NA | NA | 5.33** |
RIT Future System (MX2): Ready Spring 2020
IMSAR's ONESAR is a single-channel Ku-band radar system with a mechanical gimbal and lightweight Inertial Measurement Unit (IMU) in an extremely low-Size, Weight, and Power (SWaP) design.
Size |
W:7.2 in L: 9.02 in H: 10.1 in |
---|---|
Weight | 6 Lbs |
Power |
46 W |
Frequency | Ku |
Operating Altitude | Up to 1500 FT AGL |
Sensor Cuing | Cursor on Target |
Capabilities |
SAR |
Resolution (meters) | 0.1 |