Performance optimization and control for mission-oriented electric propulsion spacecraft

被引：0
|
作者：
Zhang Z.-L. [1 ,2 ]
Ding Y.-J. [1 ]
Yu D.-R. [1 ]
机构：
[1] Institute of Advanced Power Technology, Harbin Institute of Technology, Harbin
[2] School of Astronautics, Harbin Institute of Technology, Harbin
来源：
Ding, Yong-Jie (dingyongjie@hit.edu.cn) | 1600年 / China Spaceflight Society卷 / 37期
关键词：
Characteristic parameter; Coupling optimization control; EP spacecraft; Multimode mission; Optimal specific impulse;
D O I：
10.3873/j.issn.1000-1328.2016.08.014
中图分类号：
学科分类号：
摘要：
For coupling optimization and control of performance and mission of electric propulsion (EP), a coupling optimization method is proposed based on characteristic parameter model of EP in this paper. With the goal of maximizing the transfer rate of payload mass, the generalized rocket equation and optimal specific impulse (Isp) expressions for CP-EP combined propulsion and multimode all EP missions are deduced. Then a computing method of optimal Isp for multimode continuous EP is proposed. The effects of relevant parameters on optimal Isp are obtained based on some assumptions. The results indicate that the coupling optimization method and the formula for optimal Isp will provide theoretical guidance and generality for studying optimal Isp of multimode EP missions and coupling optimal control of EP spacecraft. © 2016, Editorial Dept. of JA. All right reserved.
引用
收藏
页码：1006 / 1014
页数：8
相关论文
共 29 条
  • [1] Woodcock G., Dankanich J., Application of solar electric propulsion to robotic and human missions in near earth space, The 42nd Joint Propulsion Conference & Exhibit, (2006)
  • [2] Garulli A., Giannitrapani A., Leomanni M., Autonomous low-earth-orbit station-keeping with electric propulsion, Journal of Guidance Control and Dynamics, 34, 6, pp. 1683-1693, (2011)
  • [3] Epenoy R., Fuel optimization for continuous-thrust orbital rendezvous with collision avoidance constraint, Journal of Guidance Control and Dynamics, 34, 2, pp. 493-503, (2011)
  • [4] Oh D.Y., Landau D., Randolph T.M., Analysis of system margins on deep space missions utilizing solar electric propulsion, The 44th Joint Propulsion Conference & Exhibit, (2008)
  • [5] Robert H.F., Advanced space propulsion for the 21st century, Journal of Propulsion Power, 19, 6, pp. 1129-1154, (2003)
  • [6] Wilson F.C., Recent advances in satellite propulsion and associated mission benefits, The 24th AIAA International Communications Satellite Systems Conference, (2006)
  • [7] Yang D.-L., Xu B., Gao Y.-T., Control method for earth satellite orbit transfer using electric propulsion, Journal of Astronautics, 36, 9, pp. 1010-1017, (2015)
  • [8] Liu T., He Z.-W., Zhao Y.-S., Continuous-thrust orbit maneuver optimization using modified robust algorithm, Journal of Astronautics, 29, 4, pp. 1216-1221, (2008)
  • [9] Oh D.Y., Analytic optimization of mixed chemical-electric orbit raising missions, The 27th International Electric Propulsion Conference, (2001)
  • [10] Oh D.Y., Randolph T., Snyder S., Optimum specific impulse profiles for mixed chemical-electric orbit raising missions, The 2th International Symposium on Low Thrust Trajectories, (2002)
123