DocumentCode
1795195
Title
Analysis and design on frozen condition of near-earth near-circluar orbit in critical inclination
Author
Wu Sheng-gang ; Qian Shan ; Li Heng-nian
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
1749
Lastpage
1753
Abstract
The frozen condition of near-earth near-circluar orbit in critical inclination was studied in this paper. The frozen theory which based on J2 and J3 earth zonal harmonics can not explain the evolvement of eccentricity and argument of periapsis in near-circluar orbit in critical inclination by factual measure data, it needs consider more higher earth zonal harmonics perturbations. At the same tine, there is the coupling phenomena exists between eccentricity and argument of periapsis. if the initial argument of periapsis is set to 180°, the change of eccentricity and argument of periapsis will appear singularity by theory analysis and numerical simulation. The eccentricity will decrease firstly and then begin to increase, and the argument of periapsis can maintain at 180° and 0°. Finally, the passive orbit control strategy and initiative orbit control strategy were put forward based on the analysis result.
Keywords
artificial satellites; celestial mechanics; control system synthesis; position control; Earth zonal harmonics perturbations; J2 Earth zonal harmonics; J3 Earth zonal harmonics; coupling phenomena; critical inclination; eccentricity evolvement; factual measure data; frozen condition; frozen theory; initiative orbit control strategy; near-Earth near-circluar orbit; numerical simulation; passive orbit control strategy; periapsis; satellite orbit; singularity; theory analysis; Couplings; Earth; Gravity; Harmonic analysis; Orbits; Satellites; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007447
Filename
7007447
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