DocumentCode :
2229648
Title :
Exploration of distant retrograde orbits for communication and observation satellites
Author :
Tan Minghu ; Zhang Ke
Author_Institution :
Sch. of Astronaut., Northwestern Polytech. Univ., Xi´an, China
fYear :
2013
fDate :
5-8 Aug. 2013
Firstpage :
1
Lastpage :
5
Abstract :
Distant retrograde orbit (DRO), serving for future astrophysical observatories and communications, has received much attention. Instead of high-order analytical approximate solutions, a new numerical method is implied for finding DRO, with a given Jacobi value. Then considering the force of Moon´s gravity, the offset of the perturbed DRO will have an impact on the accuracy of observatory and communication satellites. Hence, the initial Moon´s angle needs being considered in order to guarantee the observatory and communication accuracy.
Keywords :
Moon; celestial mechanics; numerical analysis; planetary rovers; Jacobi value; circular restricted three-body problem; communication accuracy; communication satellites; distant retrograde orbits exploration; initial Moons angle; numerical method; observation satellites; Accuracy; Earth; Jacobian matrices; Moon; Observatories; Orbits; Sun; Astrophysical satellites; accuracy; distant retrograde orbit; initial angle; numerical method;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Signal Processing, Communication and Computing (ICSPCC), 2013 IEEE International Conference on
Conference_Location :
KunMing
Type :
conf
DOI :
10.1109/ICSPCC.2013.6664014
Filename :
6664014
Link To Document :
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