Airborne topo-bathy lidar system and methods thereof
Airborne LiDAR bathymetry systems and methods of use are provided. The airborne LiDAR bathymetry system can collect topographic data and bathymetric data at high altitudes. The airborne LiDAR bathymetry system has a receiver system, a detector system, and a laser transmission system.
1. A method of aerial surveying, comprising:
mounting an airborne LiDAR bathymetry system to an aircraft, wherein the airborne LiDAR bathymetry system comprises a receiver system, a detector system, and a laser transmission system comprising beam combiner optics, wherein the receiver system comprises an objective, a reflective aperture relay, a scanning wobble mirror, and a down-collimating telescope;
flying the aircraft at an altitude of at least around 10,000 feet;
emitting from the laser transmission system a first output beam at a first wavelength;
emitting from the laser transmission system a second output beam at a second wavelength, wherein the beam combiner optics align the first output beam and the second output beam; and
collecting data by the airborne LiDAR bathymetry system.
2. The method of claim 1 , wherein the laser transmission system further comprises:
a first conditioning leg to condition the first output beam, the first conditioning leg comprising a first lens and a second lens, wherein the first lens is moveable relative to the second lens along an axis of the first output beam to adjust a beam image size of the first output beam; and
a second conditioning leg to condition the second output beam, the second conditioning leg comprising a third lens and a fourth lens, wherein the third lens is moveable relative to the fourth lens along an axis of the second output beam to adjust a beam image size of the second output beam.
3. The method of claim 1 , wherein first output beam is concentrically aligned with the second output beam.
4. The method of claim 1 , wherein the first wavelength is a 532 nm wavelength.
5. The method of claim 1 , wherein the second wavelength is a 1064 nm wavelength.
6. The method of claim 1 , wherein the detector system further comprises a plurality of additional detectors, wherein each of the plurality of detectors operates at a unique single wavelength.
7. The method of claim 1 , wherein the detector system comprises a Geiger mode array detector and a Geiger-mode avalanche photodiode (GmAPD) reformatter coupled to the Geiger mode array detector.
8. The method of claim 7 , wherein the GmAPD reformatter comprises a splitting mirror, first and second imagers, a combining mirror, and a relay imager.
9. The method of claim 1 , further comprising flying the aircraft at about 160 knots.
10. The method of claim 1 , wherein the airborne LiDAR bathymetry system has a swath width of about 850 meters.
11. The method of claim 1 , wherein the aircraft is an unmanned aerial vehicle.
12. The method of claim 1 , wherein the data is topographic data, bathymetric data, or combinations thereof.
13. A method of aerial surveying, comprising:
flying an airborne LiDAR bathymetry system at an altitude of at least around 10,000 feet, wherein the airborne LiDAR bathymetry system comprises a receiver system, a detector system, and a laser transmission system comprising a first conditioning leg for conditioning a first output beam and a second conditioning leg for conditioning a second output beam, wherein the receiver system comprises an objective, a reflective aperture relay, a scanning wobble mirror, and a down-collimating telescope;
aligning the first output beam and the second output beam with beam combiner optics;
emitting from the laser transmission system the aligned first and second output beams, wherein the first out beam is at a first wavelength and the second output beam at a second wavelength; and
collecting data by the airborne LiDAR bathymetry system.
14. The method of claim 13 , wherein aligning the first output beam and the second output beam with beam combiner optics the laser transmission system further comprises concentrically aligning the first output beam and the second output beam.
15. The method of claim 14 , wherein the first output beam has a 532 nm wavelength and the second output beam has a 1064 nm wavelength.
16. A method of aerial surveying, comprising:
mounting an airborne LiDAR bathymetry system to an aircraft;
flying the aircraft at an altitude above a sea surface;
emitting from the LiDAR bathymetry system a first output beam at a 532 nm wavelength;
emitting from the LiDAR bathymetry system a second output beam at a 1064 nm wavelength, wherein the beam combiner optics concentrically align the first output beam and the second output beam; and
collecting topographic bathymetric data by a receiver system of the airborne LiDAR bathymetry system, wherein the receiver system comprises an objective, a reflective aperture relay, a scanning wobble mirror, and a down-collimating telescope.
17. The method of claim 16 , wherein the airborne LiDAR bathymetry system comprises a detector system, and a laser transmission system, wherein the laser transmission system comprises the beam combiner optics.
18. The method of claim 16 , wherein the altitude is at least 10,000 feet.
19. The method of claim 16 , further comprising flying the aircraft at about 160 knots.
20. A method of aerial surveying, comprising:
mounting an airborne LiDAR system to an aircraft, wherein the airborne LiDAR system comprises:
(i) a laser transmission system,
(ii) a detector system comprising of a plurality of Avalanche Photodiodes (APD) supporting linear mode LiDAR and a Geiger-mode avalanche photodiode (GmAPD) coupled to a GmAPD reformatting system, and
(iii) a receiver system comprising an objective, a reflective aperture relay, a scanning wobble mirror, and a down-collimating telescope a, and;
flying the aircraft above a topographic surface;
emitting from the laser transmission system an output beam at a wavelength; and
collecting topographic data by the airborne LiDAR system.
21. The method of claim 20 , further comprising flying the aircraft above the topographic surface at about 160 knots.
22. The method of claim 20 , further comprising flying the aircraft at least 10,000 feet above the topographic surface.
23. The method of claim 20 , wherein the aircraft is an unmanned aerial vehicle.