Position and attitude control of an underactuated satellite with constant thrust

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Citations (Scopus)

Abstract

This paper discusses a position and attitude control problem of an underactuated satellite which uses on-off thruster mechanisms for control. Each thrusters has constant orientation relative to the satellite's body, and can generate only unilateral forces. The purpose of this paper is to clarify the control law for simultaneous position and attitude control for this type of satellite configuration. Considering the input constraints, we obtain the analytical solutions of the satellite's translational and rotational motion. Then the control procedure utilizing an invariant manifold is derived. Some numerical simulations are shown to verify the effectiveness of the proposed controller.

Original languageEnglish
Title of host publicationAIAA Guidance, Navigation, and Control Conference 2011
Publication statusPublished - 2011
EventAIAA Guidance, Navigation and Control Conference 2011 - Portland, OR, United States
Duration: Aug 8 2011Aug 11 2011

Other

OtherAIAA Guidance, Navigation and Control Conference 2011
CountryUnited States
CityPortland, OR
Period8/8/118/11/11

Fingerprint

Attitude control
Position control
Satellites
Controllers
Computer simulation

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

Cite this

Yoshimura, Y., Matsuno, T., & Hokamoto, S. (2011). Position and attitude control of an underactuated satellite with constant thrust. In AIAA Guidance, Navigation, and Control Conference 2011

Position and attitude control of an underactuated satellite with constant thrust. / Yoshimura, Yasuhiro; Matsuno, Takashi; Hokamoto, Shinji.

AIAA Guidance, Navigation, and Control Conference 2011. 2011.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Yoshimura, Y, Matsuno, T & Hokamoto, S 2011, Position and attitude control of an underactuated satellite with constant thrust. in AIAA Guidance, Navigation, and Control Conference 2011. AIAA Guidance, Navigation and Control Conference 2011, Portland, OR, United States, 8/8/11.
Yoshimura Y, Matsuno T, Hokamoto S. Position and attitude control of an underactuated satellite with constant thrust. In AIAA Guidance, Navigation, and Control Conference 2011. 2011
Yoshimura, Yasuhiro ; Matsuno, Takashi ; Hokamoto, Shinji. / Position and attitude control of an underactuated satellite with constant thrust. AIAA Guidance, Navigation, and Control Conference 2011. 2011.
@inproceedings{b4a46c1879e340a999216392adedf2c8,
title = "Position and attitude control of an underactuated satellite with constant thrust",
abstract = "This paper discusses a position and attitude control problem of an underactuated satellite which uses on-off thruster mechanisms for control. Each thrusters has constant orientation relative to the satellite's body, and can generate only unilateral forces. The purpose of this paper is to clarify the control law for simultaneous position and attitude control for this type of satellite configuration. Considering the input constraints, we obtain the analytical solutions of the satellite's translational and rotational motion. Then the control procedure utilizing an invariant manifold is derived. Some numerical simulations are shown to verify the effectiveness of the proposed controller.",
author = "Yasuhiro Yoshimura and Takashi Matsuno and Shinji Hokamoto",
year = "2011",
language = "English",
isbn = "9781600869525",
booktitle = "AIAA Guidance, Navigation, and Control Conference 2011",

}

TY - GEN

T1 - Position and attitude control of an underactuated satellite with constant thrust

AU - Yoshimura, Yasuhiro

AU - Matsuno, Takashi

AU - Hokamoto, Shinji

PY - 2011

Y1 - 2011

N2 - This paper discusses a position and attitude control problem of an underactuated satellite which uses on-off thruster mechanisms for control. Each thrusters has constant orientation relative to the satellite's body, and can generate only unilateral forces. The purpose of this paper is to clarify the control law for simultaneous position and attitude control for this type of satellite configuration. Considering the input constraints, we obtain the analytical solutions of the satellite's translational and rotational motion. Then the control procedure utilizing an invariant manifold is derived. Some numerical simulations are shown to verify the effectiveness of the proposed controller.

AB - This paper discusses a position and attitude control problem of an underactuated satellite which uses on-off thruster mechanisms for control. Each thrusters has constant orientation relative to the satellite's body, and can generate only unilateral forces. The purpose of this paper is to clarify the control law for simultaneous position and attitude control for this type of satellite configuration. Considering the input constraints, we obtain the analytical solutions of the satellite's translational and rotational motion. Then the control procedure utilizing an invariant manifold is derived. Some numerical simulations are shown to verify the effectiveness of the proposed controller.

UR - http://www.scopus.com/inward/record.url?scp=84878713745&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84878713745&partnerID=8YFLogxK

M3 - Conference contribution

SN - 9781600869525

BT - AIAA Guidance, Navigation, and Control Conference 2011

ER -