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Fast slew maneuvers for the High-Torque-Wheels BIROS spacecraft

Acquatella B., Paul (2018) Fast slew maneuvers for the High-Torque-Wheels BIROS spacecraft. Transactions of the Japan Society for Aeronautical and Space Sciences, 61 (2), pp. 79-86. Aerospace Technology Japan. DOI: 10.2322/tjsass.61.79 ISSN 0549-3811

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Official URL: https://www.jstage.jst.go.jp/article/tjsass/61/2/61_T-17-56/_article/-char/en

Abstract

The satellite platform BIROS is the second technology demonstrator of DLR’s ‘FireBIRD’ space mission aiming to provide infrared remote sensing for early fire detection. Among several mission goals and scientific experiments, to demonstrate a high agility attitude control system, the platform is actuated with an extra array of three orthogonal ‘HighTorque-Wheels.’ However, to enable agile reorientation, a challenge arises from the fact that time-optimal slew maneuvers are, in general, not of the Euler axis rotation type; especially whenever the actuators are constrained independently. Moreover, BIROS’ on-board computer can only accommodate rotational acceleration commands twice per second. The objective is therefore to find a methodology to design fast slew maneuvers while considering a highly dynamic plant commanded by piecewise-constant sampled-time control inputs. This is achieved by considering a comprehensive analytical nonlinear model for spacecraft equipped with reaction wheels and transcribing a time-optimal control problem formulation into a multi-criteria optimization problem. Solutions are found with a direct approach using the trajectory optimization package ‘trajOpt’ of DLR-SR’s optimization tool, Multi-Objective Parameter Synthesis (MOPS). Results based on numerical simulations are presented to illustrate this method.

Item URL in elib:https://elib.dlr.de/123142/
Document Type:Article
Additional Information:presented at ISSFD 2017, 26th International Symposium on Space Flight Dynamics. June 3-9, 2017. Matsuyama-Ehime, Japan. http://elib.dlr.de/118396/
Title:Fast slew maneuvers for the High-Torque-Wheels BIROS spacecraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Acquatella B., Paulpaul.acquatella (at) dlr.dehttps://orcid.org/0000-0002-0826-6984
Date:4 March 2018
Journal or Publication Title:Transactions of the Japan Society for Aeronautical and Space Sciences
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:61
DOI :10.2322/tjsass.61.79
Page Range:pp. 79-86
Publisher:Aerospace Technology Japan
ISSN:0549-3811
Status:Published
Keywords:Attitude Control System, Slew Maneuver Optimization, Time-Optimal Control, Sampled-Time Control
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Technik für Raumfahrtsysteme
DLR - Research theme (Project):R - Project High-Torque-Wheels
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Space System Dynamics
Deposited By: Acquatella B., Paul
Deposited On:19 Nov 2018 10:23
Last Modified:19 Nov 2018 10:23

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