Global trajectory design for position and attitude control of an underactuated satellite

Research output: Contribution to journalArticle

2 Citations (Scopus)

Abstract

Underactuated control offers fault-tolerance for satellite systems, which not only enables the position and attitude control of a satellite with fewer thrusters, but also can reduce the number of thrusters equipped on the satellite even when considering the need for backups. Due to having fewer thrusters, the coupling effect between the translational motion and rotational motion of the satellite cannot be avoided, and the coupled motion must be considered in control procedures. This paper presents a global trajectory design procedure required for the position and attitude control of an underactuated satellite. The satellite has four thrusters with constant thrust magnitudes on one plane of the satellite body. Then, an analytical solution for coupled motion between the rotation and translation of the satellite is obtained using three-step maneuvers of attitude control. The trajectory design based on the analytical solution is shown for the control of translational and rotational motion in three dimensions. Finally, a numerical simulation is performed to verify the effectiveness of the proposed design procedure.

Original languageEnglish
Pages (from-to)107-114
Number of pages8
JournalTransactions of the Japan Society for Aeronautical and Space Sciences
Volume59
Issue number3
DOIs
Publication statusPublished - Jan 1 2016

Fingerprint

attitude control
Attitude control
Position control
trajectory
Trajectories
trajectories
Satellites
translational motion
fault tolerance
backups
maneuvers
Fault tolerance
thrust
tolerance
Computer simulation

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

@article{671a2b6d16414508abe33c35e966307e,
title = "Global trajectory design for position and attitude control of an underactuated satellite",
abstract = "Underactuated control offers fault-tolerance for satellite systems, which not only enables the position and attitude control of a satellite with fewer thrusters, but also can reduce the number of thrusters equipped on the satellite even when considering the need for backups. Due to having fewer thrusters, the coupling effect between the translational motion and rotational motion of the satellite cannot be avoided, and the coupled motion must be considered in control procedures. This paper presents a global trajectory design procedure required for the position and attitude control of an underactuated satellite. The satellite has four thrusters with constant thrust magnitudes on one plane of the satellite body. Then, an analytical solution for coupled motion between the rotation and translation of the satellite is obtained using three-step maneuvers of attitude control. The trajectory design based on the analytical solution is shown for the control of translational and rotational motion in three dimensions. Finally, a numerical simulation is performed to verify the effectiveness of the proposed design procedure.",
author = "Yasuhiro Yoshimura and Takashi Matsuno and Shinji Hokamoto",
year = "2016",
month = "1",
day = "1",
doi = "10.2322/tjsass.59.107",
language = "English",
volume = "59",
pages = "107--114",
journal = "Transactions of the Japan Society for Aeronautical and Space Sciences",
issn = "0549-3811",
publisher = "Japan Society for Aeronautical and Space Sciences",
number = "3",

}

TY - JOUR

T1 - Global trajectory design for position and attitude control of an underactuated satellite

AU - Yoshimura, Yasuhiro

AU - Matsuno, Takashi

AU - Hokamoto, Shinji

PY - 2016/1/1

Y1 - 2016/1/1

N2 - Underactuated control offers fault-tolerance for satellite systems, which not only enables the position and attitude control of a satellite with fewer thrusters, but also can reduce the number of thrusters equipped on the satellite even when considering the need for backups. Due to having fewer thrusters, the coupling effect between the translational motion and rotational motion of the satellite cannot be avoided, and the coupled motion must be considered in control procedures. This paper presents a global trajectory design procedure required for the position and attitude control of an underactuated satellite. The satellite has four thrusters with constant thrust magnitudes on one plane of the satellite body. Then, an analytical solution for coupled motion between the rotation and translation of the satellite is obtained using three-step maneuvers of attitude control. The trajectory design based on the analytical solution is shown for the control of translational and rotational motion in three dimensions. Finally, a numerical simulation is performed to verify the effectiveness of the proposed design procedure.

AB - Underactuated control offers fault-tolerance for satellite systems, which not only enables the position and attitude control of a satellite with fewer thrusters, but also can reduce the number of thrusters equipped on the satellite even when considering the need for backups. Due to having fewer thrusters, the coupling effect between the translational motion and rotational motion of the satellite cannot be avoided, and the coupled motion must be considered in control procedures. This paper presents a global trajectory design procedure required for the position and attitude control of an underactuated satellite. The satellite has four thrusters with constant thrust magnitudes on one plane of the satellite body. Then, an analytical solution for coupled motion between the rotation and translation of the satellite is obtained using three-step maneuvers of attitude control. The trajectory design based on the analytical solution is shown for the control of translational and rotational motion in three dimensions. Finally, a numerical simulation is performed to verify the effectiveness of the proposed design procedure.

UR - http://www.scopus.com/inward/record.url?scp=84966526033&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84966526033&partnerID=8YFLogxK

U2 - 10.2322/tjsass.59.107

DO - 10.2322/tjsass.59.107

M3 - Article

AN - SCOPUS:84966526033

VL - 59

SP - 107

EP - 114

JO - Transactions of the Japan Society for Aeronautical and Space Sciences

JF - Transactions of the Japan Society for Aeronautical and Space Sciences

SN - 0549-3811

IS - 3

ER -