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. 23, 2018

Filed:

Feb. 19, 2016
Applicant:

Mbda Deutschland Gmbh, Schrobenhausen, DE;

Inventors:

Michael Limmer, Rehling, DE;

Thomas Gallhauser, Pfaffenhofen, DE;

Michael Alois Surauer, Chieming, DE;

Christian Surauer, Chieming, DE;

Franz Geidek, Aresing, DE;

Assignee:

MBDA Deutschland GmbH, Schrobenhausen, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F41G 7/00 (2006.01); B64C 27/08 (2006.01); G06F 17/50 (2006.01);
U.S. Cl.
CPC ...
F41G 7/002 (2013.01); B64C 27/08 (2013.01); F41G 7/001 (2013.01); F41G 7/005 (2013.01); G06F 17/5009 (2013.01);
Abstract

A stationary test device for a missile includes a retaining device for an avionics testpiece of the missile, where the retaining device enables a movement of the avionics testpiece in three rotational degrees of freedom, and a display device configured to display information on the missile surroundings, where the display device is configured to be moved inside a virtual plane by a translational carriage system. The display device can be detected by the avionics testpiece if the avionics testpiece is disposed on the retaining device. A mobile test device for the missile includes a flight platform, a carrier device mounted on the flight platform, for an avionics testpiece of the missile, wherein the carrier device enables a movement of the avionics testpiece in three rotational degrees of freedom, and a control module, where the control module is configured to control the flight platform for taking off on a specified reference trajectory, control the carrier device for orientation of the avionics testpiece, and store navigation data generated by the avionics testpiece. Finally, a test system for the missile includes the stationary test device and the mobile test device.


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