Geostationary Satellites Collocation
Autor Hengnian Lien Limba Engleză Paperback – 22 aug 2016
Hengnian Li is the Deputy Director of State Key Laboratory of Astronautic Dynamics, China.
Toate formatele și edițiile | Preț | Express |
---|---|---|
Paperback (1) | 795.89 lei 6-8 săpt. | |
Springer Berlin, Heidelberg – 22 aug 2016 | 795.89 lei 6-8 săpt. | |
Hardback (1) | 616.54 lei 6-8 săpt. | |
Springer Berlin, Heidelberg – 21 aug 2014 | 616.54 lei 6-8 săpt. |
Preț: 795.89 lei
Preț vechi: 970.60 lei
-18% Nou
Puncte Express: 1194
Preț estimativ în valută:
152.33€ • 161.73$ • 126.18£
152.33€ • 161.73$ • 126.18£
Carte tipărită la comandă
Livrare economică 25 decembrie 24 - 08 ianuarie 25
Preluare comenzi: 021 569.72.76
Specificații
ISBN-13: 9783662513163
ISBN-10: 3662513161
Pagini: 344
Ilustrații: X, 334 p. 212 illus., 12 illus. in color.
Dimensiuni: 155 x 235 x 18 mm
Greutate: 0.49 kg
Ediția:Softcover reprint of the original 1st ed. 2014
Editura: Springer Berlin, Heidelberg
Colecția Springer
Locul publicării:Berlin, Heidelberg, Germany
ISBN-10: 3662513161
Pagini: 344
Ilustrații: X, 334 p. 212 illus., 12 illus. in color.
Dimensiuni: 155 x 235 x 18 mm
Greutate: 0.49 kg
Ediția:Softcover reprint of the original 1st ed. 2014
Editura: Springer Berlin, Heidelberg
Colecția Springer
Locul publicării:Berlin, Heidelberg, Germany
Cuprins
Introduction.- Orbit Motion Foundations.- The Motion of Geostationary Satellite.- Geostationary Orbit Perturbation.- Harmonic Analysis Geostationary Orbit.- Correction Geostationary Orbit.- Maintenance Geostationary Orbit.- Collocation Prototypes and Strategies.
Textul de pe ultima copertă
Geostationary Satellites Collocation aims to find solutions for deploying a safe and reliable collocation control. Focusing on the orbital perturbation analysis, the mathematical foundations for orbit and control of the geostationary satellite are summarized. The mathematical and physical principle of orbital maneuver and collocation strategies for multi geostationary satellites sharing with the same dead band is also stressed. Moreover, the book presents some applications using the above algorithms and mathematical models to help readers master the corrective method for planning station keeping maneuvers. Engineers and scientists in the fields of aerospace technology and space science can benefit from this book.
Hengnian Li is the Deputy Director of State Key Laboratory of Astronautic Dynamics, China.
Hengnian Li is the Deputy Director of State Key Laboratory of Astronautic Dynamics, China.
Caracteristici
Focuses on the orbital perturbation analysis for the geostationary orbit
Explains mathematical and physical principle of orbital maneuver and collocation strategies
Presents applications using the algorithms and mathematical models
Includes supplementary material: sn.pub/extras
Explains mathematical and physical principle of orbital maneuver and collocation strategies
Presents applications using the algorithms and mathematical models
Includes supplementary material: sn.pub/extras
Notă biografică
Publication List:
[1] Li H. N., Geostationary Satellite Orbital Analysis and Collocation Strategies [M], Beijing: National Defense industry Press, 2010.10. [In Chinese]
[2] Li H. N., Gao Y. J., etc. the strategies and algorithms study for multi-GEO satellites collocation[J],
Journal of Astronautics, Vol. 30, No. 3:967-973. [In Chinese]
[3] Li H. N., The Separation Methods and Station Keeping Algorithms For Multi-GEOS Collocation [C], the 60th International Astronautical Congress Daejeon, Republic of Korea.
[4] Li H. N., Li J. S., on-line orbit determination method for satellite with continuous thrust acceleration [J], System Engineering and Electronics, 2010(09):1957-1961.[in Chinese]
[5] Li H. N., Li J. S., A dynamic model compensation orbit determination method for maneuvering satellite [J], Journal of Astronautics, Vol. 31, No. 10: 2269:2275.
[6] Li H. N., Li J. S., Analyzing perturbation motion and studying configuration maintenance strategy for compass-M navigation constellation, Journal of Astronautics, Vol. 31, No. 7:1756-1761. [in Chinese]
[7] Li H. N., Li J. S., on-line minimum variance estimation for thrust acceleration during orbit transfer process, Journal of Astronautics, Vol. 23, No. 5, 2002(09):76:80.
[1] Li H. N., Geostationary Satellite Orbital Analysis and Collocation Strategies [M], Beijing: National Defense industry Press, 2010.10. [In Chinese]
[2] Li H. N., Gao Y. J., etc. the strategies and algorithms study for multi-GEO satellites collocation[J],
Journal of Astronautics, Vol. 30, No. 3:967-973. [In Chinese]
[3] Li H. N., The Separation Methods and Station Keeping Algorithms For Multi-GEOS Collocation [C], the 60th International Astronautical Congress Daejeon, Republic of Korea.
[4] Li H. N., Li J. S., on-line orbit determination method for satellite with continuous thrust acceleration [J], System Engineering and Electronics, 2010(09):1957-1961.[in Chinese]
[5] Li H. N., Li J. S., A dynamic model compensation orbit determination method for maneuvering satellite [J], Journal of Astronautics, Vol. 31, No. 10: 2269:2275.
[6] Li H. N., Li J. S., Analyzing perturbation motion and studying configuration maintenance strategy for compass-M navigation constellation, Journal of Astronautics, Vol. 31, No. 7:1756-1761. [in Chinese]
[7] Li H. N., Li J. S., on-line minimum variance estimation for thrust acceleration during orbit transfer process, Journal of Astronautics, Vol. 23, No. 5, 2002(09):76:80.