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:
Dec. 19, 2017

Filed:

Mar. 28, 2013
Applicants:

Airbus Defence and Space Sas, Les Mureaux, FR;

Centre National D'etudes Spatiales Cnes, Paris, FR;

Inventors:

Renaud Broquet, Toulouse, FR;

Bernard Polle, Saint Orens de Gameville, FR;

Johan Montel, Maurens Scopont, FR;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G01S 19/55 (2010.01); G01S 3/46 (2006.01); G01S 19/54 (2010.01); G01S 3/48 (2006.01); G01S 19/53 (2010.01); G01S 5/06 (2006.01); G01S 5/02 (2010.01); G01S 19/22 (2010.01);
U.S. Cl.
CPC ...
G01S 19/55 (2013.01); G01S 3/46 (2013.01); G01S 3/48 (2013.01); G01S 19/54 (2013.01); G01S 5/0247 (2013.01); G01S 5/06 (2013.01); G01S 19/22 (2013.01); G01S 19/53 (2013.01);
Abstract

A method for calibrating spatial errors induced by phase biases having a detrimental effect on the measurements of phase differences of radio signals received by three unaligned receiving antennas of a vehicle. An inter-satellite angular deviation of a pair of satellites is estimated in two different ways: on the basis of the respective positions of the vehicle and of the satellites to obtain a theoretical inter-satellite angular deviation; and on the basis of the respective directions of incidence of the satellites relative to the vehicle, which are determined from phase measurements, to obtain an estimated inter-satellite angular deviation. The space errors are estimated on the basis of said theoretical and estimated inter-satellite angular deviations. Also, a method and system for estimating the attitude of a vehicle, in particular a spacecraft.


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