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:
Nov. 07, 2017

Filed:

Mar. 11, 2015
Applicant:

Massachusetts Institute of Technology, Cambridge, MA (US);

Inventors:

Tam Nguyen Thuc Nguyen, Cambridge, MA (US);

Kerri L. Cahoy, Lexington, MA (US);

Meghan K. Quadrino, Cambridge, MA (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/36 (2006.01); B64G 1/24 (2006.01); B64G 1/26 (2006.01); B64G 1/28 (2006.01); B64G 1/32 (2006.01); B64G 1/34 (2006.01); B64G 1/40 (2006.01);
U.S. Cl.
CPC ...
B64G 1/365 (2013.01); B64G 1/26 (2013.01); B64G 1/281 (2013.01); B64G 1/283 (2013.01); B64G 1/285 (2013.01); B64G 1/286 (2013.01); B64G 1/288 (2013.01); B64G 1/32 (2013.01); B64G 1/34 (2013.01); B64G 1/36 (2013.01); B64G 1/363 (2013.01); B64G 1/366 (2013.01); B64G 1/407 (2013.01); B64G 2001/245 (2013.01);
Abstract

Described herein are systems and methods for attitude determination using infrared Earth horizon sensors (EHSs) with Gaussian response characteristics. Attitude information is acquired by detecting Earth's infrared electromagnetic radiation and, subsequently, determining the region obscured by Earth in the sensors' fields of view to compute a nadir vector estimation in the spacecraft's body frame. The method can be applied when two sensors, each with known and distinct pointing directions, detect the horizon, which is defined as having their fields of view partially obscured by Earth. The method can be implemented compactly to provide high-accuracy attitude within small spacecraft, such as CubeSat-based satellites.


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