Attitude Maneuver and Gimbal angle guidance by SDRE controller using SGCMG integrated satellite SDLR model

Ryotaro Ozawa, Masaki Takahashi

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

Abstract

In the conventional agile attitude maneuver of a satellite, a control system of the satellite and Single Gimbal Control Moment Gyro (SGCMG) is designed separately and stability is not guaranteed under the singularity of SGCMGs. Therefore, in this research, we integrate the satellite and SGCMGs and design a model with the gimbal angular velocity as input. Since the target gimbal angle can be explicitly designed by a null motion, proposed control system is possible to guide the initial gimbal angle which is advantageous for next mission. In addition, it is shown that proposed method can guarantee stability even under the singularity of SGCMGs by the State-Dependent Riccati Equation (SDRE). Moreover, numerical simulations show that the singularity avoidance performance up to the target gimbal angle and the guidance performance of the gimbal angle are higher than the conventional method due to the optimality of gimbal angular velocity input.

Original languageEnglish
Title of host publication2017 Asian Control Conference, ASCC 2017
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1847-1852
Number of pages6
Volume2018-January
ISBN (Electronic)9781509015733
DOIs
Publication statusPublished - 2018 Feb 7
Event2017 11th Asian Control Conference, ASCC 2017 - Gold Coast, Australia
Duration: 2017 Dec 172017 Dec 20

Other

Other2017 11th Asian Control Conference, ASCC 2017
CountryAustralia
CityGold Coast
Period17/12/1717/12/20

Fingerprint

Riccati Equation
Guidance
Moment
Controller
Angle
Dependent
Singularity
Angular velocity
Control System
Target
Motion Control
Model
Null
Optimality
Integrate
Numerical Simulation

ASJC Scopus subject areas

  • Control and Optimization

Cite this

Ozawa, R., & Takahashi, M. (2018). Attitude Maneuver and Gimbal angle guidance by SDRE controller using SGCMG integrated satellite SDLR model. In 2017 Asian Control Conference, ASCC 2017 (Vol. 2018-January, pp. 1847-1852). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ASCC.2017.8287455

Attitude Maneuver and Gimbal angle guidance by SDRE controller using SGCMG integrated satellite SDLR model. / Ozawa, Ryotaro; Takahashi, Masaki.

2017 Asian Control Conference, ASCC 2017. Vol. 2018-January Institute of Electrical and Electronics Engineers Inc., 2018. p. 1847-1852.

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

Ozawa, R & Takahashi, M 2018, Attitude Maneuver and Gimbal angle guidance by SDRE controller using SGCMG integrated satellite SDLR model. in 2017 Asian Control Conference, ASCC 2017. vol. 2018-January, Institute of Electrical and Electronics Engineers Inc., pp. 1847-1852, 2017 11th Asian Control Conference, ASCC 2017, Gold Coast, Australia, 17/12/17. https://doi.org/10.1109/ASCC.2017.8287455
Ozawa R, Takahashi M. Attitude Maneuver and Gimbal angle guidance by SDRE controller using SGCMG integrated satellite SDLR model. In 2017 Asian Control Conference, ASCC 2017. Vol. 2018-January. Institute of Electrical and Electronics Engineers Inc. 2018. p. 1847-1852 https://doi.org/10.1109/ASCC.2017.8287455
Ozawa, Ryotaro ; Takahashi, Masaki. / Attitude Maneuver and Gimbal angle guidance by SDRE controller using SGCMG integrated satellite SDLR model. 2017 Asian Control Conference, ASCC 2017. Vol. 2018-January Institute of Electrical and Electronics Engineers Inc., 2018. pp. 1847-1852
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