TY - GEN
T1 - Deployment design for space platform of a space-based operationally responsive system
AU - Chang, Jianlong
AU - Zhao, Liangyu
AU - Han, Fei
N1 - Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.
PY - 2015
Y1 - 2015
N2 - Taking a space-based operationally responsive system (SORS) as background, a deployment design for space platform of a SORS is proposed and a specific way of noncoplanar orbital transfer is analyzed. Firstly, the components of the SORS are briefly introduced. According to the analysis of the time and impulse for transfer, a deployment design for space platform of a SORS is designed. Secondly a specific way of non-coplanar orbital transfer is analyzed, which is transfer at the intersection. The impulse for transfer and transfer time are optimized to be minimum at the same time, and the space launch platforms of deployed in advance in the deployment design are taken as design variable. Under the deployment design for space platform of a SORS, the results show that transfer at the intersection not only could reduce a lot of time in the SORS, but also can generate a smaller impluse.
AB - Taking a space-based operationally responsive system (SORS) as background, a deployment design for space platform of a SORS is proposed and a specific way of noncoplanar orbital transfer is analyzed. Firstly, the components of the SORS are briefly introduced. According to the analysis of the time and impulse for transfer, a deployment design for space platform of a SORS is designed. Secondly a specific way of non-coplanar orbital transfer is analyzed, which is transfer at the intersection. The impulse for transfer and transfer time are optimized to be minimum at the same time, and the space launch platforms of deployed in advance in the deployment design are taken as design variable. Under the deployment design for space platform of a SORS, the results show that transfer at the intersection not only could reduce a lot of time in the SORS, but also can generate a smaller impluse.
UR - http://www.scopus.com/inward/record.url?scp=85088354316&partnerID=8YFLogxK
U2 - 10.2514/6.2015-4498
DO - 10.2514/6.2015-4498
M3 - Conference contribution
AN - SCOPUS:85088354316
SN - 9781624103346
T3 - AIAA SPACE 2015 Conference and Exposition
BT - AIAA SPACE 2015 Conference and Exposition
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SPACE Conference and Exposition, 2015
Y2 - 31 August 2015 through 2 September 2015
ER -