Fuel-Optimal Spacecraft Cluster Flight Around an Ellipsoidal Asteroid

被引：14

作者：

Wang, Wei ^{[1
]}

Wu, Di ^{[2
]}

Lei, Hanlun ^{[3
]}

Baoyi, Hexi ^{[2
]}

机构：

[1] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China

[2] Tsinghua Univ, Sch Aerosp Engn, Beijing 100084, Peoples R China

[3] Nanjing Univ, Sch Astron & Space Sci, Nanjing 210023, Peoples R China

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2021年 / 44卷 / 10期

基金：

中国国家自然科学基金;

关键词：

RELATIVE ORBITS; MULTIPLE SPACECRAFT; FROZEN ORBITS; OPTIMIZATION; MOTION;

D O I：

10.2514/1.G005993

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1875 / 1882

页数：8

共 36 条

[1]

[Anonymous], 2000, An Introduction to the Mathematics and Methods of Astrodynamics

[2] An artificial impact on the asteroid (162173) Ryugu formed a crater in the gravity-dominated regime [J].

Arakawa, M. ;

Saiki, T. ;

Wada, K. ;

Ogawa, K. ;

Kadono, T. ;

Shirai, K. ;

Sawada, H. ;

Ishibashi, K. ;

Honda, R. ;

Sakatani, N. ;

Iijima, Y. ;

Okamoto, C. ;

Yano, H. ;

Takagi, Y. ;

Hayakawa, M. ;

Michel, P. ;

Jutzi, M. ;

Shimaki, Y. ;

Kimura, S. ;

Mimasu, Y. ;

Toda, T. ;

Imamura, H. ;

Nakazawa, S. ;

Hayakawa, H. ;

Sugita, S. ;

Morota, T. ;

Kameda, S. ;

Tatsumi, E. ;

Cho, Y. ;

Yoshioka, K. ;

Yokota, Y. ;

Matsuoka, M. ;

Yamada, M. ;

Kouyama, T. ;

Honda, C. ;

Tsuda, Y. ;

Watanabe, S. ;

Yoshikawa, M. ;

Tanaka, S. ;

Terui, F. ;

Kikuchi, S. ;

Yamaguchi, T. ;

Ogawa, N. ;

Ono, G. ;

Yoshikawa, K. ;

Takahashi, T. ;

Takei, Y. ;

Fujii, A. ;

Takeuchi, H. ;

Yamamoto, Y. .

SCIENCE, 2020, 368 (6486) :67-+

[3] Design of Bounded Relative Trajectories in the Earth Zonal Problem [J].

Baresi, Nicola ;

Scheeres, Daniel J. .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 40 (12) :3075-3087

[4] Bounded relative orbits about asteroids for formation flying and applications [J].

Baresi, Nicola ;

Scheeres, Daniel J. ;

Schaub, Hanspeter .

ACTA ASTRONAUTICA, 2016, 123 :364-375

[5] Optimal fuel-balanced impulsive formationkeeping for perturbed spacecraft orbits [J].

Beigelman, Igor ;

Gurfil, Pini .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2008, 31 (05) :1266-1283

[6]

Bryson A.E., 1975, Applied Optimal Control, P71

[7] Motion near frozen orbits as a means for mitigating satellite relative drift [J].

Gurfil, P. ;

Lara, M. .

CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2013, 116 (03) :213-227

[8] Spacecraft motion about slowly rotating asteroids [J].

Hu, W ;

Scheeres, DJ .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2002, 25 (04) :765-775

[9] Improving Low-Thrust Trajectory Optimization by Adjoint Estimation with Shape-Based Path [J].

Jiang, Fanghua ;

Tang, Gao ;

Li, Junfeng .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 40 (12) :3280-3287

[10] Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic Approach [J].

Jiang, Fanghua ;

Baoyin, Hexi ;

Li, Junfeng .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2012, 35 (01) :245-258

← 1 2 3 4 →