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References (20)
-
N. Horri, P. Palmer (2012)
Practical Implementation of Attitude-Control Algorithms for an Underactuated SatelliteJournal of Guidance Control and Dynamics, 35
-
(1995)
Anewparameterizationof the attitude kinematics -
P. Fritzson (2014)
Principles of Object-Oriented Modeling and Simulation with Modelica 3.3: A Cyber-Physical Approach -
Jaehyun Jin, Inseok Hwang (2011)
Attitude Control of a Spacecraft with Single Variable-Speed Control Moment GyroscopeJournal of Guidance Control and Dynamics, 34
-
J. Cloutier (1997)
State-dependent Riccati equation techniques: an overviewProceedings of the 1997 American Control Conference (Cat. No.97CH36041), 2
-
C. Petersen, Frederick Leve, I. Kolmanovsky (2016)
Underactuated Spacecraft Switching Law for Two Reaction Wheels and Constant Angular MomentumJournal of Guidance Control and Dynamics, 39
-
Yochoong Bang, Hyung-Don Choi (2002)
Attitude control of a bias momentum satellite using moment of inertiaIEEE Transactions on Aerospace and Electronic Systems, 38
-
Sangwon Kwon, T. Shimomura, H. Okubo (2011)
Pointing control of spacecraft using two SGCMGs via LPV control theoryActa Astronautica, 68
-
S. Kasai, H. Kojima, M. Satoh (2012)
Spacecraft attitude maneuver using two single-gimbal control moment gyrosActa Astronautica, 84
-
P. Crouch (1984)
Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body modelsIEEE Transactions on Automatic Control, 29
-
P. Tsiotras, V. Doumtchenko (2000)
CONTROL OF SPACECRAFT SUBJECT TO ACTUATOR FAILURES : STATE-OFTHE-ART AND OPEN PROBLEMS -
Tayfun Çimen (2012)
Survey of State-Dependent Riccati Equation in Nonlinear Optimal Feedback Control SynthesisJournal of Guidance Control and Dynamics, 35
-
M. Massari, M. Zamaro (2014)
Application of SDRE technique to orbital and attitude control of spacecraft formation flyingActa Astronautica, 94
-
F. Boyer, M. Alamir (2007)
Further Results on the Controllability of a Two-Wheeled SatelliteJournal of Guidance Control and Dynamics, 30
-
Robert Williams, D. Lawrence (2007)
Linear State-Space Control Systems -
S. Rhee, H. Ko, Woo-Young Jang, Jun-Won Son (2009)
Roll/Yaw Momentum Management Method of Pitch Momentum Biased SpacecraftJournal of The Korean Society for Aeronautical & Space Sciences, 37
-
H. Krishnan, N. McClamroch, M. Reyhanoglu (1993)
Attitude stabilization of a rigid spacecraft using two momentum wheel actuatorsJournal of Guidance Control and Dynamics, 18
-
R. Ozawa, Masaki Takahashi (2018)
Agile Attitude Control and Singularity Avoidance/Escape by the SDRE Method Using a Biased State-Dependent Weighting MatrixApplied Sciences, 8
-
J. Chaurais, H. Ferreira, J. Ishihara, R. Borges (2015)
Attitude Control of an Underactuated Satellite Using Two Reaction WheelsJournal of Guidance Control and Dynamics, 38
-
Hyungjoo Yoon, Panagiotis Tsiotras (2006)
Spacecraft Line-of-Sight Control Using a Single Variable-Speed Control Moment GyroJournal of Guidance Control and Dynamics, 29
- Publisher
- Springer Journals
- Copyright
- Copyright © 2018 by The Korean Society for Aeronautical & Space Sciences and Springer Nature Singapore Pte Ltd.
- Subject
- Engineering; Aerospace Technology and Astronautics; Fluid- and Aerodynamics
- ISSN
- 2093-274X
- eISSN
- 2093-2480
- DOI
- 10.1007/s42405-018-0104-5
- Publisher site
- See Article on Publisher Site
Abstract
This paper deals with the attitude control problem of an underactuated satellite controlled by two reaction wheels. The angular momentum of the satellite is assumed to be non-zero or biased. Under these conditions, rotation to arbitrary attitude (roll, pitch, and yaw) is not possible, but direction or limited attitude control (roll and pitch) is possible. For such control, a nonlinear controller is proposed to utilize the angular momentum as gyroscopic torque. The controller is designed using the State-Dependent Riccati Equation (SDRE) method. This SDRE method provides a systematic way to design nonlinear controllers for diverse combinations of two reaction wheels. The proposed method has been verified by numerical simulations and the designed control system works satisfactorily.
Journal
International Journal of Aeronautical & Space Sciences – Springer Journals
Published: Nov 10, 2018