Airborne Laser Scanner with Online Waveform Processing ® RIEGL VQ-480i • high-accuracy ranging based on echo digitization and online waveform processing • high laser repetition rate fast data acquisition The V-Line® Airborne Laser Scanner RIEGL VQ-480i provides high speed data acquisition using a narrow infrared laser beam and a fast line scanning mechanism. High-accuracy laser ranging is based on RIEGL´s unique echo digitization and online waveform processing, which allows achieving superior measurement results even under adverse atmospheric conditions, and the evaluation of multiple target echoes. • multiple target capability unlimited number of targets The scanning mechanism is based on a fast rotating multi-facet poly- • perfectly linear scan lines lines. • compact, rugged, and lightweight design The RIEGL VQ-480i is a very compact and lightweight scanner, moun- • electrical interfaces for GPS data string and Sync Pulse (1PPS) helicopters or UAVs. The instrument requires only one power supply and • mechanical interface for IMU mounting gonal mirror, which provides fully linear, unidirectional and parallel scan table in any orientation and even under limited space conditions on provides line scan data via the integrated LAN-TCP/IP interface. The binary data stream can easily be decoded by user-designed software making use of the available software library RiVLib. • integrated LAN-TCP/IP interface Typical applications include • Corridor Mapping • Power Line Inspection • Cultural Heritage Mapping visit our website www.riegl.com Airborne Laser Scanning Technical Data RIEGL VQ®-480i Laser Product Classification Class 1 Laser Product according to IEC60825-1:2007 The following clause applies for instruments delivered into the United States: Complies with 21 CFR 1040.10 and 1040.11 except for deviations pursuant to Laser Notice No. 50, dated June 24, 2007. Range Measurement Performance Measuring Principle Laser Pulse Repetition Rate PRR 1) Effective Measurement Rate (meas./sec.) 1) 2) Max. Measuring Range 3) 4) natural targets ≥ 20 % natural targets ≥ 60 % Max. Operating Flight Altitude AGL 1) 2) time of flight measurement, echo signal digitization, online waveform processing, multiple-time-around-processing 50 kHz 25 000 100 kHz 50 000 400 kHz 200 000 550 kHz 275 000 1300 m 2100 m 1050 m (3450 ft) 950 m 650 m 550 m 500 m 1550 m 1100 m 950 m 800 m 750 m 550 m 450 m 400 m (2450 ft) (1800 ft) (1450 ft) (1300 ft) practically unlimited (details on request) 400 m 700 m 300 m (1000 ft) Max. Number of Targets per Pulse 200 kHz 100 000 300 kHz 150 000 1) Rounded values. 2) Reflectivity ≥ 20%, ±30° FOV, additional roll angle ±5°. 3) Typical values for average conditions. Maximum range is specified for flat targets with size in excess of the laser beam diameter, perpendicular angle of incidence, and for atmospheric visibility of 23 km. In bright sunlight, the max. range is shorter than under overcast sky. 4) Ambiguity to be resolved by post-processing with RiMTA ALS software. Minimum Range Accuracy 5) 7) Precision 6) 7) Laser Pulse Repetition Rate 1) 8) Max. Effective Measurement Rate 1) Echo Signal Intensity Laser Wavelength Laser Beam Divergence 9) Laser Beam Footprint (Gaussian Beam Definition) 5) 6) Accuracy is the degree of conformity of a measured quantity to its actual (true) value. Precision, also called reproducibility or repeatability, is the degree to which further measurements show the same result. Scanner Performance 7) 8) 9) One sigma @ 150 m range under RIEGL test conditions. User selectable. Measured at the 1/e2 points. 0.30 mrad corresponds to an increase of 30 mm of beam diameter per 100 m distance. Scanning Mechanism Field of View (selectable) Scan Speed (selectable) Angular Step Width (selectable) rotating polygon mirror 60° (+30° / -30°) 10 - 150 scans/sec 0.002° ≤ ≤ 0.36° Angle Measurement Resolution Internal Sync Timer Scan Sync (optional) 0.001° for real-time synchronized time stamping of scan data scanner rotation synchronization between consecutive laser shots Data Interfaces Configuration Scan Data Output GPS-System Mechanical Interfaces Mounting of the Laser Scanner Mounting of IMU sensor General Technical Data Power Supply Input Voltage Current Consumption Main Dimensions Weight Humidity Protection Class Max. Flight Altitude (operating) Max. Flight Altitude (not operating) Temperature Range 2 10 m 20 mm 20 mm up to 550 kHz up to 275 000 meas./sec. (@ 550 kHz PRR & 60° FOV) for each echo signal, high-resolution 16 bit intensity information is provided near infrared 0.3 mrad 31 mm @ 100 m, 75 mm @ 250 m, 150 mm @ 500 m LAN 10/100/1000 Mbit/sec LAN 10/100/1000 Mbit/sec, USB 2.0 Serial RS232 interface for data string with GPS-time information, TTL input for 1PPS synchronization pulse mounting base block (with 8 x M8 thread inserts and 6x mounting slots) 3 x M6 thread inserts in the front and rear plate (rigidly coupled with the internal mechanical structure) 18 - 32 V DC typ. 65 W 360.5 x 206 x 219 mm (L x W x H) approx. 11.5 kg max. 80 % non condensing @ +31°C IP64, dust and splash-proof 16 500 ft (5 000 m) above MSL 18 000 ft (5 500 m) above MSL -10°C up to +40°C (operation) / -20°C up to +50°C (storage) Maximum Measurement Range & Point Density RIEGL VQ®-480i PRR = 50 kHz PRR = 50 kHz WHUUDFRWWD 960 880 250 15 20 25 30 35 40 FOLIIVVDQGPDVRQU\ FRQVWUXFWLRQFRQFUHWH 500 10 4500 70 45 50 55 60 65 70 75 80 85 800 720 640 560 480 4 3500 3000 2500 2000 10 150 320 1000 160 80 0 0 90 20 WHUUDFRWWD >IW@ 5000 1360 MTA2 1200 40 45 50 55 60 65 70 75 4500 80 85 800 720 640 560 480 70 8 3500 3000 2500 2000 10 00 6 150 1500 250 400 320 1000 160 80 20 0 ft 40 30 50 60 70 ([DPSOH ([DPSOH FOLIIVVDQGPDVRQU\ 40 45 50 55 60 35 Flight Altitude AGL 500 ft (152 m) 700 ft (213 m) 1000 ft (305 m) 1800 ft (549 m) 30 4500 50 4000 25 80 90 100 VQ-480i VQ-480i at at 10SXOVHVVHFRQG 10SXOVHVVHFRQG $OWLWXGH $OWLWXGH IW$*/6SHHG IW$*/6SHHG 0NQ 0NQ RHVXOWLQJ3RLQW'HQVLW\aSWPð RHVXOWLQJ3RLQW'HQVLW\aSWPð 65 70 75 880 80 85 800 720 640 560 480 3000 2500 2000 ft 1500 70 20 10 15 10 180 00 0f t ft 0 ft 400 320 1000 5 240 160 500 80 0 90 7DUJHW5HÀHFWLYLW\>@ MTA1: no ambiguity / 1 transmitted pulse „in the air” MTA2: 2 transmitted pulses „in the air” 0 swath width 176 m 246 m 352 m 634 m 3500 3RLQW'HQVLW\ [SWVP2] 960 MTA2 2SHUDWLQJ)OLJKW$OWLWXGH$*/ FRQVWUXFWLRQFRQFUHWH WHUUDFRWWD 35 5000 1040 ZKLWHSODVWHUZRUNOLPHVWRQH 30 >IW@ 1120 ZKLWHPDUEOH 25 [m] 1520 1200 250 20 0 ft 1280 MTA1 15 ft 0 0 1360 500 10 swath width 246 m 352 m 528 m 880 m t 1440 750 5 0f @ visibility 23 km @ visibility 15 km @ visibility 8 km 1000 0 VQ-480i at 5SXOVHVVHFRQG $OWLWXGH IW$*/6SHHG 0NQ RHVXOWLQJ3RLQW'HQVLW\aSWPð 6SHHG [NQ] 1250 0 100 PRR = 200 kHz GHFLGXRXVWUHHV GU\DVSKDOW FRQLIHULRXVWUHHV GU\VQRZ ZHWLFHEODFNWDUSDSHU Maximum Measurement Range [m] 1500 90 500 90 2500 1750 80 2 240 PRR = 200 kHz 2000 70 4 7DUJHW5HÀHFWLYLW\>@ MTA1: no ambiguity / 1 transmitted pulse „in the air” MTA2: 2 transmitted pulses „in the air” 2250 60 Flight Altitude AGL 700 ft (213 m) 1000 ft (305 m) 1500 ft (457 m) 2500 ft (762 m) 10 4000 3RLQW'HQVLW\ [SWVP2] ZKLWHSODVWHUZRUNOLPHVWRQH 35 ZKLWHPDUEOH 30 MTA1 FOLIIVVDQGPDVRQU\ FRQVWUXFWLRQFRQFUHWH 250 25 12 1120 500 20 50 ([DPSOH 1280 880 15 40 30 1440 2SHUDWLQJ)OLJKW$OWLWXGH$*/ GHFLGXRXVWUHHV GU\DVSKDOW FRQLIHULRXVWUHHV GU\VQRZ ZHWLFHEODFNWDUSDSHU Maximum Measurement Range [m] [m] 1520 960 10 ft 500 1040 750 5 3500 1 PRR = 100 kHz 1000 0 0 ft 2 @ visibility 23 km @ visibility 15 km @ visibility 8 km 1250 0 ft 1500 240 2500 1500 t 400 PRR = 100 kHz 1750 0f swath width 246 m 352 m 528 m 1232 m 6SHHG [NQ] MTA1: no ambiguity / 1 transmitted pulse „in the air” 2000 00 3 7DUJHW5HÀHFWLYLW\>@ 2250 Flight Altitude AGL 700 ft (213 m) 1000 ft (305 m) 1500 ft (457 m) 3500 ft (1078 m) 5 4000 3RLQW'HQVLW\ [SWVP2] MTA1 750 5 6 1120 2SHUDWLQJ)OLJKW$OWLWXGH$*/ GU\DVSKDOW 1200 1040 1000 0 5000 1280 1250 0 >IW@ 1360 ZKLWHSODVWHUZRUNOLPHVWRQH 1500 [m] 1520 1440 ZKLWHPDUEOH 1750 GHFLGXRXVWUHHV Maximum Measurement Range [m] 2000 GU\VQRZ 2250 FRQLIHULRXVWUHHV ZHWLFHEODFNWDUSDSHU 2500 0 20 30 40 50 60 70 80 90 100 6SHHG [NQ] @ visibility 23 km @ visibility 15 km @ visibility 8 km ([DPSOH VQ-480i at 20SXOVHVVHFRQG $OWLWXGH IW$*/6SHHG 0NQ RHVXOWLQJ3RLQW'HQVLW\aSWPð The following conditions are assumed for the Operating Flight Altitude AGL • ambiguity resolved by multiple-time-around (MTA) processing & flight planning • target size ≥ laser footprint • scan angle 60° • average ambient brightness • roll angle +/-5° 3 Maximum Measurement Range & Point Density RIEGL VQ®-480i PRR = 300 kHz PRR = 300 kHz [m] >IW@ 1520 5000 1360 1200 880 800 720 560 480 MTA2 250 0 0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 3500 30 3000 25 2500 2000 500 5 0 0 80 90 ZKLWHSODVWHUZRUNOLPHVWRQH >IW@ 5000 1360 1200 800 720 250 MTA1 25 30 35 40 45 50 55 60 65 70 75 80 80 320 3500 3000 2500 2000 160 50 1000 20 500 10 0 0 20 ZKLWHSODVWHUZRUNOLPHVWRQH >IW@ 5000 1360 1200 t 00 ft 40 30 50 60 70 90 100 ([DPSOH VQ-480i at 40SXOVHVVHFRQG $OWLWXGH IW$*/6SHHG 0NQ RHVXOWLQJ3RLQW'HQVLW\aSWPð MTA1 35 40 45 50 55 60 65 70 75 120 Flight Altitude AGL 300 ft (92 m) 500 ft (152 m) 700 ft (213 m) 1000 ft (305 m) 30 800 720 ft swath width 106 m 176 m 246 m 352 m 3500 3000 2500 2000 1500 3RLQW'HQVLW\ [SWVP2] 880 0 4000 80 85 320 50 80 70 60 10 00 0f 0f t t ft 40 1000 240 160 20 500 80 0 90 7DUJHW5HÀHFWLYLW\>@ MTA1: no ambiguity / 1 transmitted pulse „in the air” MTA2: 2 transmitted pulses „in the air” MTA3: 3 transmitted pulses „in the air” MTA4: 4 transmitted pulses „in the air” 140 100 1040 960 ZKLWHPDUEOH 250 0 20 30 40 50 60 70 ([DPSOH @ visibility 23 km @ visibility 15 km @ visibility 8 km • ambiguity resolved by multiple-time-around (MTA) processing & flight planning • target size ≥ laser footprint • scan angle 60° 80 90 6SHHG [NQ] VQ-480i at 55SXOVHVVHFRQG $OWLWXGH IW$*/6SHHG 0NQ RHVXOWLQJ3RLQW'HQVLW\aSWPð The following conditions are assumed for the Operating Flight Altitude AGL 4 80 400 MTA2 30 4500 1120 560 MTA3 25 t 1280 640 500 20 0f 0f 1440 2SHUDWLQJ)OLJKW$OWLWXGH$*/ FOLIIVVDQGPDVRQU\ FRQVWUXFWLRQFRQFUHWH WHUUDFRWWD GHFLGXRXVWUHHV GU\DVSKDOW FRQLIHULRXVWUHHV GU\VQRZ ZHWLFHEODFNWDUSDSHU Maximum Measurement Range [m] [m] 1520 480 15 swath width 106 m 176 m 282 m 457 m PRR = 550 kHz MTA4 10 80 13 30 90 750 5 ft @ visibility 23 km @ visibility 15 km @ visibility 8 km 1000 0 VQ-480i at 30SXOVHVVHFRQG $OWLWXGH IW$*/6SHHG 0NQ RHVXOWLQJ3RLQW'HQVLW\aSWPð 6SHHG [NQ] 1250 0 100 40 80 2500 1500 50 60 1500 PRR = 550 kHz 1750 90 240 85 MTA1: no ambiguity / 1 transmitted pulse „in the air” MTA2: 2 transmitted pulses „in the air” MTA3: 3 transmitted pulses „in the air” 2000 0 4000 7DUJHW5HÀHFWLYLW\>@ 2250 80 400 ZKLWHPDUEOH 500 30 3RLQW'HQVLW\ [SWVP2] 880 480 20 70 70 1040 960 Flight Altitude AGL 300 ft (92m) 500 ft (152 m) 800 ft (244 m) 1300 ft (396 m) 90 4500 1120 640 MTA2 100 1280 2SHUDWLQJ)OLJKW$OWLWXGH$*/ FOLIIVVDQGPDVRQU\ FRQVWUXFWLRQFRQFUHWH WHUUDFRWWD GHFLGXRXVWUHHV GU\DVSKDOW FRQLIHULRXVWUHHV GU\VQRZ ZHWLFHEODFNWDUSDSHU Maximum Measurement Range [m] [m] 1520 560 15 60 ([DPSOH 1440 750 10 50 PRR = 400 kHz MTA3 5 40 30 20 @ visibility 23 km @ visibility 15 km @ visibility 8 km 1000 0 ft 15 6SHHG [NQ] 1250 0 ft 1000 160 2500 1500 00 t 240 PRR = 400 kHz 1750 15 00 0f t 10 320 85 MTA1: no ambiguity / 1 transmitted pulse „in the air” MTA2: 2 transmitted pulses „in the air” 2000 10 20 7DUJHW5HÀHFWLYLW\>@ 2250 70 0f swath width 176 m 246 m 352 m 528 m 1500 400 ZKLWHPDUEOH MTA1 35 3RLQW'HQVLW\ [SWVP2] 1040 640 500 50 4000 1120 960 Flight Altitude AGL 500 ft (152 m) 700 ft (213 m) 1000 ft (305 m) 1500 ft (457 m) 40 4500 1280 1000 750 45 1440 2SHUDWLQJ)OLJKW$OWLWXGH$*/ MTA3 1250 ZKLWHSODVWHUZRUNOLPHVWRQH WHUUDFRWWD GU\DVSKDOW FOLIIVVDQGPDVRQU\ 1500 FRQVWUXFWLRQFRQFUHWH 1750 GHFLGXRXVWUHHV Maximum Measurement Range [m] 2000 GU\VQRZ 2250 FRQLIHULRXVWUHHV ZHWLFHEODFNWDUSDSHU 2500 • average ambient brightness • roll angle +/-5° 100 Dimensional Drawings RIEGL VQ®-480i 5 Example for a profile of scan data processed in MTA zones 1 to 4 Multiple-time-around Data Acquisition and Processing In time-of-flight laser ranging a maximum unambiguous measurement range exists, which is defined by the laser pulse repetition rate and the speed of light. In case the echo signal of an emitted laser pulse arrives later than the emission of the subsequently emitted laser pulse, the range result becomes ambiguous - an effect known as „Multiple-Time-around“ (MTA). The RIEGL VQ-480i allows ranging beyond the maximum unambiguous measurement range using a sophisticated modulation scheme applied to the train of emitted laser pulses. The dedicated post-processing software RiMTA ALS provides algorithms for multiple-time-around processing, which automatically assign definite range results to the correct MTA zones without any further user interaction required. Example for a profile of scan data processed in MTA zones 1 to 4 RIEGL Laser Measurement Systems GmbH Riedenburgstraße 48 3580 Horn, Austria Phone: +43 2982 4211 | Fax: +43 2982 4210 office@riegl.co.at www.riegl.com RIEGL USA Inc. Orlando, Florida | info@rieglusa.com | www.rieglusa.com RIEGL Japan Ltd. Tokyo, Japan | info@riegl-japan.co.jp | www.riegl-japan.co.jp RIEGL China Ltd. Beijing, China | info@riegl.cn | www.riegl.cn www.riegl.com Information contained herein is believed to be accurate and reliable. However, no responsibility is assumed by RIEGL for its use. Technical data are subject to change without notice. Data Sheet, RIEGL VQ-480i, 2015-03-24