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:
Feb. 26, 2019

Filed:

Sep. 07, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Stuart R. Kobata, Huntington Beach, CA (US);

Martin Edward Lozano, Huntington Beach, CA (US);

Henry Rodriguez, Jr., Diamond Bar, CA (US);

Kevin Swenson, Huntington Beach, CA (US);

Brian Vaniman, Huntington Beach, CA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 39/02 (2006.01); G01M 99/00 (2011.01); G05D 1/10 (2006.01); B64F 5/60 (2017.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64F 5/60 (2017.01); G01M 99/004 (2013.01); G05D 1/102 (2013.01); B64C 2201/127 (2013.01); B64C 2201/128 (2013.01);
Abstract

A system and method for collecting test data from a unit under test (UUT) in a multi-gravity environment is disclosed. In one embodiment, the method comprises determining a desired accelerative load profile for the UUT, determining the commanded flight profile of a flight vehicle at least in part from the desired accelerative load profile and a predicted dynamic response of the flight vehicle having the UUT mounted thereto to the commanded flight profile, commanding the flight vehicle having the UUT mounted thereto to fly the determined flight profile, and collecting the test data using a data acquisition system communicatively coupled to the UUT.


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