The design of transfer trajectory for Ivar asteroid exploration mission
The design of transfer trajectory for Ivar asteroid exploration mission
复制标题
Ivar小行星探测任务转移轨迹设计
DOI:
10.1016/j.actaastro.2009.04.006
复制
发表时间:
2009-12
影响因子:
3.5
通讯作者:
乔栋
中科院分区:
文献类型:
--
作者:
乔栋
An impending demand for exploring the small bodies, such as the comets and the asteroids, envisioned the Chinese Deep Space exploration mission to the Near Earth asteroid Ivar. A design and optimal method of transfer trajectory for asteroid Ivar is discussed in this paper. The transfer trajectory for rendezvous with asteroid Ivar is designed by means of Earth gravity assist with deep space maneuver (Delta-VEGA) technology. A Delta-VEGA transfer trajectory is realized by several trajectory segments, which connect the deep space maneuver and swingby point. Each trajectory segment is found by solving Lambert problem. Through adjusting deep maneuver and arrival time, the match condition of swingby is satisfied. To reduce the total mission velocity increments further, a procedure is developed which minimizes total velocity increments for this scheme of transfer trajectory for asteroid Ivar. The trajectory optimization problem is solved with a quasi-Newton algorithm utilizing analytic first derivatives, which are derived from the transversality conditions associated with the optimization formulation and primer vector theory. The simulation results show the scheme for transfer trajectory causes C3 and total velocity increments decrease of 48.80% and 13.20%, respectively.
登录
查看更多内容
影响因子:
2.6
作者:
M. Hechler
通讯作者:
M. Hechler
DOI:
--
发表时间:
2003
期刊:
--
影响因子:
--
作者:
Cui Ping-yuan;Liao Li-tao
通讯作者:
Cui Ping-yuan;Liao Li-tao
DOI:
--
发表时间:
1988
期刊:
--
影响因子:
--
作者:
C. G. Sauer
通讯作者:
C. G. Sauer
影响因子:
2.6
作者:
J. Sims;J. Longuski;Andrew J. Staugler
通讯作者:
J. Sims;J. Longuski;Andrew J. Staugler
影响因子:
6.8
作者:
J. Meditch
通讯作者:
J. Meditch