- About EITEE
- Articles Online
- For Authors
- For Reviewers
- Features
- Subscription & Service
- Personal Center
- Logout
FOLLOWUS
- About EITEE
- Introduction
- Editorial Board
- Corresponding Experts
- Events
- Honors
- Contact Us
- Articles Online
- Current Issue
- Archive
- Special Issues
- Virtual Issues
- Highlights
- In Press
- For Authors
- Submit
- Call for papers
- Guide for Authors
- Ethics & Disclosures
- Fee & Funding
- Downloads
- For Reviewers
- Guide for Reviewers
- Ethics & Disclosures
- Thanks card
- Features
- FITEE Forum
- Engineering Front
- Paper Videos
- Editors’ Corner
- Other Resources
- Subscription & Service
- Subscription
- Services
Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations
- Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations
- Frontiers of Information Technology & Electronic Engineering Vol. 13, Issue 5, Pages: 328-338(2012)
- Affiliations：
1.National Key Laboratory of Inertial Technology, Beihang University, Beijing 100191, China
2.Novel Inertial Instrument & Navigation System Technology Key Laboratory of Fundamental Science for National Defense, Beihang University, Beijing 100191, China
- Author bio：
Ke SUN, kekeesun81@aspe.buaa.edu.cn
- Funds：
DOI：10.1631/jzus.C1100350
CLC： V529.1;TP13Received：28 November 2011，
Revised：2012-;4-;9，
Published：2012-05
- Accepted：
Scan QR Code
Jian-cheng FANG, Ke SUN. Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(5): 328-338.
Jian-cheng FANG, Ke SUN. Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(5): 328-338. DOI： 10.1631/jzus.C1100350.
摘要
Abstract
Maintenance of high performance formation control is important for low Earth orbit (LEO) formation missions of small spacecraft. In this paper
a model of nonlinear relative motion dynamics is built
and then nonlinear and important perturbations affecting the formation configuration
such as
J
2
and atmospheric drag
are analyzed as disturbances. Global navigation satellite system based relative positioning with nonlinear filtering is adopted to provide state information associated with the perturbations. By combining disturbance observer based control with
H
∞
state feedback
a composite disturbance attenuation controller is proposed for maintenance of continuous and accurate formation. With consideration of precise control relying on micro thrusters
a composite disturbance attenuation based saturated controller is designed and its stability is proved. Finally
through numerical simulations
we demonstrate that control accuracy is improved after effectively avoiding perturbations and that stabilization can be satisfied using this method.
关键词
Keywords
references
K.T. Alfriend , , , H. Schaub , , , D.W. Gim . . Gravitational Perturbations, Nonlinearity and Circular Orbit Assumption Effect on Formation Flying Control Strategies . . American Astronautical Society Guidance & Control Conf., AAS 00-012 , , 2000 . . p.1 - - 20 . . . .
P.J. Buist , , , P.J.G. Teunissen , , , S. Verhagen , , , G. Giorgi . . A vectorial bootstrapping approach for integrated GNSS-based relative positioning and attitude determination of spacecraft . . Acta Astron. , , 2011 . . 68 ( ( 7-8 ): ): 1113 - - 1125 . . DOI: 10.1016/j.actaastro.2010.09.027 http://doi.org/10.1016/j.actaastro.2010.09.027 . .
E. Canuto . . Embedded model control: outline of the theory . . ISA Trans. , , 2007 . . 46 ( ( 3 ): ): 363 - - 377 . . DOI: 10.1016/j.isatra.2007.01.006 http://doi.org/10.1016/j.isatra.2007.01.006 . .
E. Canuto , , , A. Molano-Jimenez , , , C. Perez-Montenegro , , , L. Massotti . . Long-distance, drag-free, low-thrust, LEO formation control for Earth gravity monitoring . . Acta Astron. , , 2011 . . 69 ( ( 7-8 ): ): 571 - - 582 . . DOI: 10.1016/j.actaastro.2011.04.018 http://doi.org/10.1016/j.actaastro.2011.04.018 . .
W.H. Clohessy , , , R.S. Wiltshire . . Terminal guidance system for satellite rendezvous . . J. Aerosp. Sci. , , 1960 . . 27 ( ( 9 ): ): 653 - - 658 . . . .
C.E. de Souza , , , L. Xie . . On the discrete-time bounded real lemma with application in the characterization of static state feedback H ∞ controllers . . Syst. Control Lett. , , 1992 . . 18 ( ( 1 ): ): 61 - - 71 . . DOI: 10.1016/0167-6911(92)90108-5 http://doi.org/10.1016/0167-6911(92)90108-5 . .
J.C. Fang , , , X.L. Gong . . Predictive iterated Kalman filter for INS/GPS integration and its application to SAR motion compensation . . IEEE Trans. Instrum. Meas. , , 2010 . . 59 ( ( 4 ): ): 909 - - 915 . . DOI: 10.1109/TIM.2009.2026614 http://doi.org/10.1109/TIM.2009.2026614 . .
L. Guo , , , W.H. Chen . . Disturbance attenuation and rejection for systems with nonlinearity via DOBC approach . . Int. J. Rob. Nonl. Control , , 2005 . . 15 ( ( 3 ): ): 109 - - 125 . . DOI: 10.1002/rnc.978 http://doi.org/10.1002/rnc.978 . .
L. Guo , , , C.B. Feng , , , W.H. Chen . . A survey of disturbance-observer-based control for dynamic nonlinear system . . Dynam. Cont. Discr. Impul. Syst. , , 2006 . . 13 79 - - 84 . . . .
K. Han , , , W. Hao , , , Z.H. Jin . . Magnetometer-only linear attitude estimation for bias momentum pico-satellite . . J. Zhejiang Univ.-Sci. A (Appl. Phys. & Eng.) , , 2010 . . 11 ( ( 6 ): ): 455 - - 464 . . DOI: 10.1631/jzus.A0900725 http://doi.org/10.1631/jzus.A0900725 . .
P. Massioni , , , T. Keviczky , , , E. Gill , , , M. Verhaegen . . A decomposition-based approach to linear time-periodic distributed control of satellite formations . . IEEE Trans. Control Syst. Technol. , , 2011 . . 19 ( ( 3 ): ): 481 - - 492 . . DOI: 10.1109/TCST.2010.2051228 http://doi.org/10.1109/TCST.2010.2051228 . .
H. Schaub , , , S.R. Vadali , , , J.L. Junkins , , , K.T. Alfriend . . Spacecraft formation flying control using mean orbit elements . . J. Astron. Sci. , , 2000 . . 48 ( ( 1 ): ): 69 - - 87 . . . .
D. Sun , , , F.Q. Zhou , , , J. Zhou . . Robust control for multiple spacecraft flying . . J. Proj. Rock. Miss. Guid. , , 2004 . . 24 ( ( 2 ): ): 279 - - 281 . . . .
S.S. Vaddi , , , S.R. Vadali , , , K.T. Alfriend . . Formation flying: accommodating nonlinearity and eccentricity perturbations . . J. Guid. Control Dyn. , , 2003 . . 26 ( ( 2 ): ): 214 - - 223 . . DOI: 10.2514/2.5054 http://doi.org/10.2514/2.5054 . .
Z.K. Wang , , , Y.L. Zhang . . Design and verification of a robust formation keeping controller . . Acta Astron. , , 2007 . . 61 ( ( 7-8 ): ): 565 - - 574 . . DOI: 10.1016/j.actaastro.2007.01.064 http://doi.org/10.1016/j.actaastro.2007.01.064 . .
L.M.B. Winternitz , , , W.A. Bamford , , , G.W. Heckler . . A GPS receiver for high-altitude satellite navigation . . IEEE J. Sel. Top. Signal Process. , , 2009 . . 3 ( ( 4 ): ): 541 - - 556 . . DOI: 10.1109/JSTSP.2009.2023352 http://doi.org/10.1109/JSTSP.2009.2023352 . .
E. Wnuk , , , J. Golebiewska . . Relative satellite motion in a formation . . Adv. Space Res. , , 2007 . . 40 ( ( 1 ): ): 35 - - 42 . . DOI: 10.1016/j.asr.2007.01.049 http://doi.org/10.1016/j.asr.2007.01.049 . .
G.Y. Xu , , , D.W. Wang . . Nonlinear dynamic equations of satellite relative motion around an oblate Earth . . J. Guid. Control Dyn. , , 2008 . . 31 ( ( 5 ): ): 1521 - - 1524 . . DOI: 10.2514/1.33616 http://doi.org/10.2514/1.33616 . .
S. Yoon , , , J.B. Lundberg . . Euler angle dilution of precision in GPS attitude determination . . IEEE Trans. Aerosp. Electron. Syst. , , 2001 . . 37 ( ( 3 ): ): 1077 - - 1083 . . DOI: 10.1109/7.953258 http://doi.org/10.1109/7.953258 . .
Z.H. You , , , B. Li , , , Z.H. Dong . . Status and key technologies of spacecraft formation on Sun-Earth Lagrange point . . Aerosp. China , , 2005 . . 5 ( ( 7 ): ): 27 - - 31 . . . .
J.X. Zhang , , , X.B. Cao , , , J.H. Wang , , , X.H. Lin . . Configuration, orbit design of InSAR formation based on mean elements . . IEEE Trans. Aerosp. Electron. Syst. , , 2009 . . 45 ( ( 2 ): ): 747 - - 752 . . DOI: 10.1109/TAES.2009.5089555 http://doi.org/10.1109/TAES.2009.5089555 . .
Y.L. Zhang , , , G.Q. Zeng , , , Z.K. Wang . . Theories and Applications of Distributed Satellites System . . Science Publishing Company, Beijing (in Chinese) , , 2008 . . .
J.F. Li , , , X. Meng , , , Y.F. Gao , , , X. Li . . Study on relative orbital configuration in satellite formation flying . . Acta Mech. Sin. , , 2005 . . 21 ( ( 1 ): ): 87 - - 94 . . DOI: 10.1007/s10409-004-0009-3 http://doi.org/10.1007/s10409-004-0009-3 . .
H.P. Liu , , , F.C. Sun , , , Y.N. Hu . . H-infinity control for fuzzy singularly perturbed systems . . Fuzzy Sets Syst. , , 2005 . . 155 ( ( 2 ): ): 272 - - 291 . . DOI: 10.1016/j.fss.2005.05.004 http://doi.org/10.1016/j.fss.2005.05.004 . .
H.P. Liu , , , F.C. Sun , , , Z.Q. Sun . . Stability analysis and synthesis of fuzzy singularly perturbed systems . . IEEE Trans. Fuzzy Syst. , , 2005 . . 13 ( ( 2 ): ): 273 - - 284 . . DOI: 10.1109/TFUZZ.2004.839660 http://doi.org/10.1109/TFUZZ.2004.839660 . .
S.A. Schweighart , , , R.J. Sedwick . . Cross-track of satellite formations in the presence of J2 disturbances . . J. Guid. Control Dyn. , , 2005 . . 28 ( ( 4 ): ): 824 - - 826 . . DOI: 10.2514/1.12387 http://doi.org/10.2514/1.12387 . .
K. Xiong , , , H. Zhang , , , L. Liu . . Adaptive robust extended Kalman filter for nonlinear stochastic systems . . IET Control Theory Appl. , , 2008 . . 2 ( ( 3 ): ): 239 - - 250 . . DOI: 10.1049/iet-cta:20070096 http://doi.org/10.1049/iet-cta:20070096 . .
- L-PDFDownload
- Meta-XMLDownload
- BibTeXDownload
- EndnoteDownload
- RefMan Download
- NoteExpressDownload
- NoteFirstDownload
Publicity Resources
Related Articles
Related Author
Related Institution
Chat- Address：Zhejiang University Press, 148 Tianmushan Road, Hangzhou, China Postal code：310028
- Tel：+86-571-88273162 Email：fitee@zju.edu.cn
- Copyright © 2000 - 2025, Zhejiang University Press 京ICP备09064830号-19
京公网安备11010802024621 - It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
- Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.
