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:
Jan. 06, 2015

Filed:

May. 31, 2012
Applicants:

Priyavadan Mamidipudi, Bristow, VA (US);

Elizabeth A. Dakin, Great Falls, VA (US);

Daniel C. Dakin, Great Falls, VA (US);

Philip L. Rogers, Hume, VA (US);

Edgar K. Dede, Manassas, VA (US);

Peter Gatchell, Nokesville, VA (US);

Madhukiran Panabakam, Herndon, VA (US);

Lance Leclair, Manassas, VA (US);

Chia-chen Chang, Gaithersburg, MD (US);

Rupak Changkakoti, Haymarket, VA (US);

Inventors:

Priyavadan Mamidipudi, Bristow, VA (US);

Elizabeth A. Dakin, Great Falls, VA (US);

Daniel C. Dakin, Great Falls, VA (US);

Philip L. Rogers, Hume, VA (US);

Edgar K. Dede, Manassas, VA (US);

Peter Gatchell, Nokesville, VA (US);

Madhukiran Panabakam, Herndon, VA (US);

Lance Leclair, Manassas, VA (US);

Chia-Chen Chang, Gaithersburg, MD (US);

Rupak Changkakoti, Haymarket, VA (US);

Assignee:

Optical Air Data Systems, LLC, Manassas, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01S 17/95 (2006.01); B64C 19/00 (2006.01); G01S 17/50 (2006.01); G01S 17/88 (2006.01); G01S 17/58 (2006.01); G05D 1/10 (2006.01);
U.S. Cl.
CPC ...
B64C 19/00 (2013.01); G01S 17/50 (2013.01); G01S 17/88 (2013.01); G01S 17/58 (2013.01); G01S 17/95 (2013.01); G05D 1/105 (2013.01);
Abstract

A method of using a light detection system for increasing the accuracy of a precision airdrop is described. Radiation is transmitted to target areas between an airborne vehicle and a dropzone target. Scattered radiation is received from the target areas. Respective wind characteristics are determined from the scattered radiation and a wind velocity map is generated, based on the respective wind characteristics, between the airborne vehicle, and at least the dropzone target. An aerial release point for the precision airdrop is computed based on the generated wind velocity map and a location of the dropzone target.


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