Abstract
The origins, types, and application purposes of space object orbital data are introduced, where the applications of space object orbital data in target conjunction assessments and space situational analyses are emphasized.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Liou JC (2014) Satellite box score. Orbital Debris Q News 18(1):9
Hash Y, Bean NP, Steyn WH et al (1998) Attitude control recovery of the CERISE microsatellite following an in–orbit collision. Adv Astronaut Sci 98:655–663
Johnson N (1996) First natural collision of cataloged earth satellites. Orbital Debris Q News 1(2):1–2
Liou JC (2005) Accidental collisions of cataloged satellites identified. Orbital Debris Q News 9(2):1
Liou JC (2009) Satellite collision leaves significant debris clouds. Orbital Debris Q News 13(2):1
Joint chiefs of staff (2013) Space operations. Joint Publication 3–14. May 29th 2013
Liu ZG (2000) Design of low orbit space target surveillance net. J Spacecraft TT&C Technol 19(4):9–17
Qiao K, Wang ZL, Cong MY (2006) Comparison and Analysis on space-based and ground-based surveillance systems of space objects. Opt Tech 32(5):744–749
Burnham WF, Morton FE, Sridharan R et al (2000) Mission planning for space—based surveillance with the space-based visible sensor. J Guid Control Dyn 23(1):165–169
Liu L (2000) Orbit theory of spacecraft. National Defense Industry Press, Beijing
Hoots FR, Roehrich RL (1980) Space track report no 3: models for propagation of NORAD element sets. Aerospace Defense Command, Peterson, pp 1–79
Hoots FR, Schumacher PW, Glover RA (2004) History of analytical orbit modeling in the U. S. space surveillance system. J Guidance Control Dyn 27(2):174–185
Vallado DA, Crawford P, Hujsak R (2006) Revisiting spacetrack no 3. In: AIAA/AAS astrodynamics specialist conference and exhibit, AIAA 2006-6753, Keystone, Colorado
Li JS (2003) Orbit determination of spacecrafts. National Defense Industry Press, Beijing
Vallado DA (2005) An analysis of state vector propagation using differing flight dynamics programs, AAS 05-199. In: space flight mechanics conference AAS/AIAA, Copper Mountain, Colorado
Fonte DJ (1996) Comparison of orbit propagation in the research and development Goddard trajectory determination system. Adv Astronaut Sci 90(2):1–949
Wu LD (2011) Orbits and detections of man-made satellites and space debris. Science and Technology Press of China, Beijing
Gavin RT (2010) NASA’ s orbital debris conjunction assessment and collision avoidance strategy, JSC-CN-19799. NASA Johnson Space Center Flight Dynamics Division, Houston
Newman L K, Duncan M (2006) Establishment and implementation of a close approach evaluation and avoidance process for Earth observing system missions. In: astrodynamics specialist conference and exhibit AIAA 2006–6291, AIAA/AAS Aug 21–24 2006, Keystone, Colorado
Kelso T S, Alfano S (2005) Satellite orbital conjunction reports assessing threatening encounters in space (SOC-RATES). AAS 05-124. In: 15th AAS/AIAA space flight mechanics conference, Copper Mountain, Colorado
Klinkrad H, Alarcon J R, Sanchez N (2005) Collision avoidance for operational ESA satellite. In: Proceedings of the fourth european conference on space debris Darmstadt, Germany
Alarcon – Rodriguez JR, Martinez – Fadrique FM, Klinkrad H (2004) Development of a collision risk assessment tool. Adv Space Res 34:1120–1124
Flohrer T, Krag H, Klinkrad H (2009) ESA’s process for the identification and assessment of high—risk con-junction events. Adv Space Res 44:355–363
Laporte F, Sasot E (2008) Operational management of collision risks for LEO satellites at CNES. In: AIAA 2008-3409 SpaceOps 2008 conference, Heidelberg, Germany
Aida S, Kirschner M, Wermuth M, et al (2010) Collision avoidance operations for LEO satellites controlled by GSOC. In: AIAA 2010-2298. SpaceOps 2010 conference, Huntsville, Alabama
Matsuda I, Hirose C, Kudo N (2010) The JAXA conjunction assessment process. In: AIAA 2010-2039. SpaceOps 2010 conference, Huntsville, Alabama
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2017 National Defense Industry Press, Beijing and Springer Nature Singapore Pte Ltd.
About this chapter
Cite this chapter
Chen, L., Bai, XZ., Liang, YG., Li, KB. (2017). Introduction. In: Orbital Data Applications for Space Objects. Springer, Singapore. https://doi.org/10.1007/978-981-10-2963-9_1
Download citation
DOI: https://doi.org/10.1007/978-981-10-2963-9_1
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-10-2962-2
Online ISBN: 978-981-10-2963-9
eBook Packages: EngineeringEngineering (R0)