TY - JOUR
T1 - A novel orbit deployment method for lifting reentry delivery system
AU - Yao, Wei
AU - Luo, Jian Jun
AU - Fang, Qun
PY - 2014/9/30
Y1 - 2014/9/30
N2 - In this paper,we focus on the difference between the deployment problems of the novel lifting reentry delivery system and the traditional constellation. The sub-satellite point track model, the coverage band model and the coverage criterion model are established to simulate the performance of the orbit deployment. To conquer the limitation of the nonhomogeneity of the traditional deployment method, an improved double inclination band method is presented, and numerical simulations are carried out to justify its validity. The simulation result shows that the present method has a superior performance than the traditional one in that it both accomplishes the global coverage mission and enhances the coverage dimension of important area by about 20 percent.
AB - In this paper,we focus on the difference between the deployment problems of the novel lifting reentry delivery system and the traditional constellation. The sub-satellite point track model, the coverage band model and the coverage criterion model are established to simulate the performance of the orbit deployment. To conquer the limitation of the nonhomogeneity of the traditional deployment method, an improved double inclination band method is presented, and numerical simulations are carried out to justify its validity. The simulation result shows that the present method has a superior performance than the traditional one in that it both accomplishes the global coverage mission and enhances the coverage dimension of important area by about 20 percent.
KW - Constellation design
KW - Double inclination band method
KW - Orbit deployment
KW - Reentry delivery system
UR - http://www.scopus.com/inward/record.url?scp=84907953458&partnerID=8YFLogxK
U2 - 10.3873/j.issn.1000-1328.2014.09.002
DO - 10.3873/j.issn.1000-1328.2014.09.002
M3 - 文章
AN - SCOPUS:84907953458
SN - 1000-1328
VL - 35
SP - 992
EP - 999
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 9
ER -