Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels)
This paper studies model predictive control (MPC) for spacecraft nonlinear attitude control with actuator input nonlinearities. This technology is important to achieve high-rate large angle attitude maneuver problems of recent spacecraft missions. To this end, we first derive linear matrix inequalit...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | Japanese |
| Published: |
The Japan Society of Mechanical Engineers
2016-10-01
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| Series: | Nihon Kikai Gakkai ronbunshu |
| Subjects: | |
| Online Access: | https://www.jstage.jst.go.jp/article/transjsme/82/842/82_16-00198/_pdf/-char/en |
| _version_ | 1797989142883205120 |
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| author | Atsushi SAKAMOTO Yuichi IKEDA Isao YAMAGUCHI Takashi KIDA |
| author_facet | Atsushi SAKAMOTO Yuichi IKEDA Isao YAMAGUCHI Takashi KIDA |
| author_sort | Atsushi SAKAMOTO |
| collection | DOAJ |
| description | This paper studies model predictive control (MPC) for spacecraft nonlinear attitude control with actuator input nonlinearities. This technology is important to achieve high-rate large angle attitude maneuver problems of recent spacecraft missions. To this end, we first derive linear matrix inequality (LMI) conditions to ensure input-to-state stability (ISS) or asymptotic stability (AS) of MPC closed-loop systems for standard actuators such as reaction control systems (RCS) and reaction wheels (RW). After providing optimization algorithms based on branch and bound methods, we evaluate and compare the control performance of each case using RW, RCS and both RCS and RW in combination through numerical simulations for astronomical observation satellite. |
| first_indexed | 2024-04-11T08:15:29Z |
| format | Article |
| id | doaj.art-0791b1c3e69d440080a2ae9be8069d2c |
| institution | Directory Open Access Journal |
| issn | 2187-9761 |
| language | Japanese |
| last_indexed | 2024-04-11T08:15:29Z |
| publishDate | 2016-10-01 |
| publisher | The Japan Society of Mechanical Engineers |
| record_format | Article |
| series | Nihon Kikai Gakkai ronbunshu |
| spelling | doaj.art-0791b1c3e69d440080a2ae9be8069d2c2022-12-22T04:35:11ZjpnThe Japan Society of Mechanical EngineersNihon Kikai Gakkai ronbunshu2187-97612016-10-018284216-0019816-0019810.1299/transjsme.16-00198transjsmeNonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels)Atsushi SAKAMOTO0Yuichi IKEDA1Isao YAMAGUCHI2Takashi KIDA3University of Electro-Communications, Department of Mechanical Engineering and Intelligent SystemsShonan Institute of Technology, Department of Mechanical EngineeringNational Defense Academy, Department of Aerospace EngineeringUniversity of Electro-Communications, Department of Mechanical Engineering and Intelligent SystemsThis paper studies model predictive control (MPC) for spacecraft nonlinear attitude control with actuator input nonlinearities. This technology is important to achieve high-rate large angle attitude maneuver problems of recent spacecraft missions. To this end, we first derive linear matrix inequality (LMI) conditions to ensure input-to-state stability (ISS) or asymptotic stability (AS) of MPC closed-loop systems for standard actuators such as reaction control systems (RCS) and reaction wheels (RW). After providing optimization algorithms based on branch and bound methods, we evaluate and compare the control performance of each case using RW, RCS and both RCS and RW in combination through numerical simulations for astronomical observation satellite.https://www.jstage.jst.go.jp/article/transjsme/82/842/82_16-00198/_pdf/-char/enguidance and controlspacecraft attitude controlmodel predictive controloptimality and stabilityinput saturationquantized inputs |
| spellingShingle | Atsushi SAKAMOTO Yuichi IKEDA Isao YAMAGUCHI Takashi KIDA Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels) Nihon Kikai Gakkai ronbunshu guidance and control spacecraft attitude control model predictive control optimality and stability input saturation quantized inputs |
| title | Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels) |
| title_full | Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels) |
| title_fullStr | Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels) |
| title_full_unstemmed | Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels) |
| title_short | Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels) |
| title_sort | nonlinear model predictive control applied to spacecraft attitude control closed loop stability and optimality with thrusters and wheels |
| topic | guidance and control spacecraft attitude control model predictive control optimality and stability input saturation quantized inputs |
| url | https://www.jstage.jst.go.jp/article/transjsme/82/842/82_16-00198/_pdf/-char/en |
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