IP Library › Granted Patent US 11,542,035
Granted Patent B2
US 11,542,035 · App. 16/953,752 · Granted Jan 3, 2023

Spectral camera control device, spectral camera control system, storage medium storing spectral camera control program, and network system for distributing spectral camera control program

Inventors: Yukihiro Takahashi (Sapporo, JP); Junichi Kurihara (Sapporo, JP); Tetsuro Ishida (Sapporo, JP)
Assignee: NATIONAL UNIVERSITY CORPORATION HOKKAIDO UNIVERSITY
B64D47/08B64C27/04B64C39/02G01J3/027G01J3/0278G01J3/0289G01J3/12G01J3/2823G01J3/32G01J3/51G01N21/31G02F1/13G02F1/133509G01J2003/1213G01J2003/1269G01J2003/283G01J2003/284G01J2003/2826G01N2021/1797G01N2201/0214
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,542,035
App. No.
16/953,752
Granted
Jan 3, 2023
Kind
B2
Abstract

A spectral camera control device, being installed, along with a spectral camera provided with a liquid crystal tunable filter, in an aircraft capable of stationary flight. The spectral camera control device causes the spectral camera to capture a spectral image in a snapshot mode each time a transmission wavelength of the liquid crystal tunable filter is switched while the aircraft is in stationary flight, and the spectral camera control device causes a plurality of spectral images to be captured in succession at a same transmission wavelength when an SN ratio of the captured spectral image is less than a predetermined threshold.

Claims (36)

1. A spectral camera control device, being installed, along with a spectral camera provided with a liquid crystal tunable filter, in an aircraft capable of stationary flight, wherein

the spectral camera control device causes the spectral camera to capture a spectral image in a snapshot mode each time a transmission wavelength of the liquid crystal tunable filter is switched while the aircraft is in stationary flight, and

the spectral camera control device causes a plurality of spectral images to be captured in succession at a same transmission wavelength when an SN ratio of the captured spectral image is less than a predetermined threshold.

2. The spectral camera control device according to claim 1 , wherein

a number of the spectral images to be captured in succession at a same transmission wavelength is calculated by Formula (2) shown below:

N >(SN t /SN1) 2   Formula (2)

where each symbol represents the following:

N: Number of spectral images to be captured,

SN1:SN ratio of first spectral image, and

SNt:SN ratio threshold.

3. A spectral camera control system comprising:

the spectral camera control device according to claim 1 ; and

a spectral camera to be controlled by the spectral camera control device.

4. An aircraft capable of stationary flight, wherein

the spectral camera control system according to claim 3 is installed therein.

5. A non-transitory storage medium storing a spectral camera control program, being installed, along with a spectral camera provided with a liquid crystal tunable filter, in an aircraft capable of stationary flight, wherein

the spectral camera control program causes a computer to function as a spectral camera control device which causes the spectral camera to capture a spectral image in a snapshot mode each time a transmission wavelength of the liquid crystal tunable filter is switched while the aircraft is in stationary flight, and

the spectral camera control program causes the computer to function as the spectral camera control device which causes a plurality of spectral images to be captured in succession at a same transmission wavelength when an SN ratio of the captured spectral image is less than a predetermined threshold.

6. The non-transitory storage medium according to claim 5 , wherein

the spectral camera control program causes a computer to function as a spectral camera control device which calculates a number of spectral images to be captured in succession at a same transmission wavelength by Formula (2) shown below:

N >(SN t /SN1) 2   Formula (2)

where each symbol represents the following:

N: Number of spectral images to be captured,

SN1:SN ratio of first spectral image, and

SNt:SN ratio threshold.

7. A distributing method for the spectral camera control program, which is stored in the non-transitory storage medium according to claim 5 , through a network, the distributing method comprising:

a step of distributing the spectral camera control program to a terminal computer connected to the network.

8. A network system for distributing a spectral camera control program, being installed, along with a spectral camera provided with a liquid crystal tunable filter, in an aircraft capable of stationary flight, the network system comprising:

a server, and

a terminal computer that is connected to the server through a network, wherein

the control program comprises

the spectral camera control program causes a computer of the aircraft to function as a spectral camera control device which causes the spectral camera to capture a spectral image in a snapshot mode each time a transmission wavelength of the liquid crystal tunable filter is switched while the aircraft is in stationary flight, and

the spectral camera control program causes the computer to function as the spectral camera control device which causes a plurality of spectral images to be captured in succession at a same transmission wavelength when an SN ratio of the captured spectral image is less than a predetermined threshold.

9. A spectral image capturing method for capturing an spectral image utilizing a spectral camera control device which is installed, along with a spectral camera provided with a liquid crystal tunable filter, in an aircraft capable of stationary flight, the method with the spectral camera control device comprising:

causing the spectral camera to capture a spectral image in a snapshot mode each time a transmission wavelength of a liquid crystal tunable filter is switched while the aircraft is in stationary flight, and

causing the spectral camera to capture a plurality of spectral images in succession at a same transmission wavelength when an SN ratio of the captured spectral image is less than a predetermined threshold.

Priority Claims (1)
JP 2016-080896 · Apr 14, 2016 · national
Continuity (2)
Division 16093624
Related Publication 20210114748A1 · Apr 22, 2021