MicroSAVI-2C hyperspectral imaging instrument

NegotiableUpdate on 01/13

Model

Nature of the Manufacturer: Producers

Product Category

Place of Origin

Online Consult

Overview

MicroSAVI-2C hyperspectral imaging instrument

Product Details

microSAVI-2C（400-2500 nm）
spectrum	Visible light and near-infrared	so-Shortwave infrared
Sensor type	Push sweep type	Push sweep type
performance
Spectral range (continuous)	400-1000nm	950-2500nm
#Number of spectral channels	288	256
#Number of lateral pixels	1920 (1840 effective)±5%	640±3%
Total field of view angle	36.6°±1°40°±2	40°±2
Instantaneous field of view angle	0.36 mRad (0.021°)	1.09 mRad
f/#	f/2.5	f/2.5
Spectral sampling width/line	2.1nm average	6.1nm average
spectral resolution	<>	<9nm>9nm>
dynamic range	12-bits	14-bits
Maximum frame rate	83 fps	100 fps
Data recording capacity	2 TB (SSD,SATA III)	2 TB (SSD, SATA III)
Data recording capability (hours)	5 hours @83 fps	10 hours @100 fps
Data rate	92 MB/s	33 MB/s
Pixel size (micrometers)	5.86 x 5.86	15 X 15
Panoramic electronic count (single pixel)	30,000 electrons	>500 000 electrons
power	~110W
Suggested environmental restrictions
Operating temperature	environment -10°to +40°C (+14°to +104°F) RH 20-50%non-condensing
Maximum height	4,420m (14,500 ft) ASL
Storage temperature	optimum -20°to +60°C (-4°to +140°F) RH 10-90%non-condensing

P/N	explain
02104501	ITRESNavigation module（15L）-Performance specifications1（RMSError in the application of autonomous vehicles
	SPS	DGPS2	RTK3	Post-Processed4
Position (m)	1.5 – 3.0	0.5 – 2.0	0.02 – 0.05	0.02 – 0.05
Speed (m/s)	0.05	0.05	0.02	0.015
Roll and pitch (deg)	0.04	0.03	0.03	0.025
True heading3 （deg）	0.03	0.28	0.18	0.08
1 Typical performance. The actual results depend on the structure of the satellite, atmospheric conditions, and other environmental factorsinfluence. 2 Typical task outline, maximum root mean square error. During low-speed rotor applications and hovering, heading errors will increase. 3 Requires base station and radio connection, sold separately. 4 POSPacDrones and short base operation specifications are subject to change without prior notice.

93004500

1 POSPacLicense for drone post-processing software

•advancedApplanix IN-FusionTM GNSSInertial integration technology

•useApplanix SmartCalTMSolid state compensation technologyMEMSInertial sensor

•advancedTrimble MaxwellcustomizedGNSSMeasurement technology

• 336A channel(GPS, GLONASS, BeiDou, Galileo, QZSS, SBAS, Trimble RTX, Omnistar)

• IMUData rate200Hz

• 100HzPosition, roll, pitch, and heading outputs

•Internally recorded6GBFlash memory, external recording to miniature imaging device

•No export license required

•Supports many unmanned aerial vehicle LiDAR systems, includingRiegl VUX、mini-VUX、Velodyne Puck、Puck-Lite, andTeledyne Optech CL-90

come fromITRESThe navigation data (position, attitude, heading) of the navigation system is directly recorded onto the onboard micro imaging systemSSDUp, then process it as a differentialSBETSolution,In order to inputITRES GCSSGeographic correction software.Accurate timing recording is used to synchronize the navigation solution with the frame data of the imager, while performing aperture correction andDSMTo generate stitched images or individual flight routes that have been geocorrected and orthorectified.