The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 13, 2019

Filed:

Aug. 28, 2015
Applicant:

Spookfish Innovations Pty Ltd, Bentley, Western Australia, AU;

Inventors:

Simon Cope, Burswood, AU;

Michael von Bertouch, Bicton, AU;

Assignee:

Spookfish Innovagtions PTY LTD, Bentley, Western Australia, AU;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 11/02 (2006.01); G05D 1/00 (2006.01); G01S 19/51 (2010.01); G08G 5/00 (2006.01); G08G 5/04 (2006.01); G03B 15/00 (2006.01); G06K 9/00 (2006.01);
U.S. Cl.
CPC ...
G01C 11/02 (2013.01); G01S 19/51 (2013.01); G03B 15/006 (2013.01); G05D 1/0055 (2013.01); G06K 9/0063 (2013.01); G08G 5/0021 (2013.01); G08G 5/0052 (2013.01); G08G 5/0086 (2013.01); G08G 5/045 (2013.01);
Abstract

An aerial survey image capture system for a survey aircraft is disclosed. The system comprises a camera system arranged to capture successive images of ground beneath a survey aircraft. The camera system has associated camera parameters, and a loss of separation (LOS) avoidance system for a survey aircraft. The LOS avoidance system is arranged to determine a predicted closest point of approach (CPA) distance between the survey aircraft and the nearby aircraft based on their locations and movements, compare the CPA distance with a defined minimum separation distance corresponding to a LOS, and determine an estimate for at least one navigation parameter of the survey aircraft required for the CPA distance to remain above the defined minimum separation distance. The system is further arranged to modify camera system parameters so as to at least partially compensate for a change in survey efficiency when the estimated at least one navigation parameter is used to navigate the survey aircraft.


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