Fuel-Optimal Predictive Control of Satellite Formation Keeping Based on Genetic Algorithm

被引：0
|
作者：
Xu, Nuo [1 ]
Lin, Jinxing [1 ]
Miao, Yuhang [1 ]
Wu, Edmond Qi [2 ]
机构：
[1] Nanjing Univ Posts & Telecommun, Coll Automat, Nanjing, Jiangsu, Peoples R China
[2] Shanghai Jiao Tong Univ, Minist Educ, Key Lab Syst Control & Informat Proc, Shanghai, Peoples R China
来源：
2019 IEEE 28TH INTERNATIONAL SYMPOSIUM ON INDUSTRIAL ELECTRONICS (ISIE) | 2019年
基金：
中国国家自然科学基金;
关键词：
satellite formation; fuel-optimal; economic model predictive control; genetic algorithm; penalty function method; SPACECRAFT FORMATION; ECONOMIC MPC; OPTIMIZATION;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
This paper addresses the keeping control problem of the leader-follower satellite formation by using an economic model predictive control method. The objective function in the designed economic model predictive control is comprised of two parts. One part is an adjustment term which is used to realize the trajectory tracking. The other part is an economic term l(e). which achieves fuel optimization. In addition, genetic algorithm is used to solve the control law which realizes the keeping control of satellite formation. Simulation results show that the proposed control method can achieve fuel optimization control for satellite formation.
引用
收藏
页码：527 / 532
页数：6
相关论文
共 50 条
  • [1] Model Predictive Control for Satellite Formation Keeping Based n Genetic Algorithm
    Xu, Nuo
    Lin, Jinxing
    Miao, Yuhang
    Gao, Zhifeng
    PROCEEDINGS OF THE 2019 31ST CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2019), 2019, : 1918 - 1923
  • [2] Predictive control for satellite formation keeping
    He Donglei & Cao Xibin Research Center of Satellite Technology
    Journal of Systems Engineering and Electronics, 2008, (01) : 161 - 166
  • [3] Predictive control for satellite formation keeping
    He Donglei
    Cao Xibin
    JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2008, 19 (01) : 161 - 166
  • [4] Fuel-optimal eccentricities for precise formation keeping of spacecraft on Keplerian orbits
    Yamada, Katsuhiko
    Kimura, Masaya
    Jikuya, Ichiro
    ACTA ASTRONAUTICA, 2011, 68 (11-12) : 1811 - 1819
  • [5] SECOND-ORDER ANALYTICAL SOLUTION TO FUEL-OPTIMAL CONTROL PROBLEMS IN SATELLITE FORMATION FLYING
    Lee, Sangjin
    Park, Sang-Young
    SPACEFLIGHT MECHANICS 2010, PTS I-III, 2010, 136 : 933 - 948
  • [6] FUEL-OPTIMAL CONTROL METHOD OF HOVERING FORMATION INITIALIZATION AND RECONFIGURATION
    Rao, Yinrui
    Chen, Huan
    Han, Chao
    ASTRODYNAMICS 2018, PTS I-IV, 2019, 167 : 3169 - 3184
  • [7] Fuel-optimal satellite formation reconfiguration method with best passive safety parameters
    Zeng, Qiaoling
    Zhu, Xiaoyu
    Wang, Jihe
    ADVANCES IN SPACE RESEARCH, 2024, 74 (02) : 987 - 1000
  • [8] Fuel-Optimal Geometric Path Planning Algorithm for Spacecraft Formation Flying
    Kaptui Sipowa, Hermann
    McMahon, Jay
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2022, 45 (10) : 1862 - 1872
  • [9] Fuel-optimal control of CVT powertrains
    Pfiffner, R
    Guzzella, L
    Onder, CH
    ADVANCES IN AUTOMOTIVE CONTROL 2001, 2001, : 17 - 22
  • [10] Design of an efficient algorithm for fuel-optimal look-ahead control
    Hellstrom, Erik
    Aslund, Jan
    Nielsen, Lars
    CONTROL ENGINEERING PRACTICE, 2010, 18 (11) : 1318 - 1327
12345