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. 29, 2020

Filed:

Aug. 10, 2017
Applicant:

Mitsubishi Electric Research Laboratories, Inc., Cambridge, MA (US);

Inventors:

Avishai Weiss, Cambridge, MA (US);

David Zlotnik, Ann Arbor, MI (US);

Stefano Di Cairano, Newton, MA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/24 (2006.01); B64G 1/00 (2006.01); B64G 1/26 (2006.01); B64G 1/28 (2006.01);
U.S. Cl.
CPC ...
B64G 1/244 (2019.05); B64G 1/00 (2013.01); B64G 1/242 (2013.01); B64G 1/26 (2013.01); B64G 1/28 (2013.01); B64G 1/283 (2013.01); B64G 1/285 (2013.01); B64G 1/286 (2013.01); B64G 2001/245 (2013.01);
Abstract

A control system for controlling an operation of a spacecraft. A model predictive controller (MPC) produces a solution for controlling thrusters of the spacecraft. The MPC optimizes a cost function over a finite receding horizon using a model of dynamics of the spacecraft effecting a pose of the spacecraft and a model of dynamics of momentum exchange devices of the spacecraft effecting an orientation of the spacecraft. The optimization is subject to hard and soft constraints on angles of thrusts generated by thrusters. Further, the hard constraints require the angles of thrusts in the solution to fall within a predetermined range defined by the hard constraints. The soft constraints penalize the solution for deviation of the angles of thrusts from nominal angles corresponding to a torque-free thrust passing through the center of the mass of the spacecraft. A thruster controller operates the thrusters according to the solution of the MPC.


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