Distributed control of spacecraft formation under J2 perturbation in the port-Hamiltonian framework

被引:0
|
作者
Hao, Wenkang [1 ]
Chen, Qifeng [1 ]
Wei, Caisheng [1 ]
Liao, Yuxin [1 ]
机构
[1] Cent South Univ, Sch Automat, Changsha 410083, Peoples R China
关键词
Port-Hamiltonian system; J; 2; perturbation; Nonlinear model; Spacecraft formation; Distributed; Passive control; PASSIVITY-BASED CONTROL;
D O I
10.1016/j.asr.2024.08.061
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
To control the relative position and relative velocity of spacecraft formation, a time-varying nonlinear relative motion model under J 2 perturbation in an elliptical orbit is established in the port-Hamiltonian (PH) framework, and a distributed control law for spacecraft formation is developed using the consensus algorithm for parameter estimation and the passivity-based control (PBC) method based on the state-error interconnection and damping assignment (IDA) technique. First, the influence of J 2 perturbation on the potential energy and orbit parameters in the model is considered when the relative motion model is built in the PH frame, and the expression of the relative motion acceleration under J 2 perturbation is given. Second, to solve the problem that the state of the chief spacecraft cannot be directly obtained from the deputy spacecraft under distributed communication, a consensus-based parameter estimation method is introduced, the estimated parameter of the chief spacecraft is applied to the relative motion model in the PH frame, and a state error model with the estimated parameters derived from the consistency algorithm is established. Then, after the stability analysis is conducted on the desired PH system containing the estimated parameter values, the desired Hamiltonian energy function with the estimated parameters is designed according to the time-varying errors of the relative equilibrium states of the deputy spacecraft and the errors between deputy spacecraft, and the distributed control law of spacecraft formation is derived based on the state-error IDA-PBC method. Finally, the expected relative motion trajectory designed based on the TH equation is used to simulate a spacecraft formation under J 2 perturbation, and the results indicate that the spacecraft can quickly converge to the expected formation under the influence of the control law. (c) 2024 COSPAR. Published by Elsevier B.V. All rights are reserved, including those for text and data mining, AI training, and similar technologies.
引用
收藏
页码:5767 / 5778
页数:12
相关论文
共 50 条
  • [41] Satellite formation keeping using differential lift and drag under J2 perturbation
    Shao, Xiaowei
    Song, Mingxuan
    Wang, Jihe
    Zhang, Dexin
    Chen, Junli
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2017, 89 (01): : 11 - 19
  • [42] Distributed control of UAVs formation based on port⁃Hamiltonian system
    Hao W.
    Bao S.
    Chen Q.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2023, 44
  • [43] Higher Order Sliding Mode Control of Formation Flying Satellites with J2 Perturbation
    Li Yafei
    Liu Xiangdong
    Xiao Yuzhi
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 643 - 648
  • [44] Relative motion control for formation flying satellite constellations in the presence of J2 perturbation
    Zhang, Hong-Hua
    Zhang, Guo-Feng
    Lin, Lai-Xing
    Yuhang Xuebao/Journal of Astronautics, 2003, 24 (05):
  • [45] Reduced order in domain control of distributed parameter port-Hamiltonian systems via energy shaping
    Liu, Ning
    Wu, Yongxin
    Le Gorrec, Yann
    Lefevre, Laurent
    Ramirez, Hector
    AUTOMATICA, 2024, 161
  • [46] Minimum control for spacecraft formations in a J2 perturbed environment
    Sabatini, M.
    Izzo, D.
    Palmerini, G. B.
    CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2009, 105 (1-3): : 141 - 157
  • [47] Minimum control for spacecraft formations in a J2 perturbed environment
    M. Sabatini
    D. Izzo
    G. B. Palmerini
    Celestial Mechanics and Dynamical Astronomy, 2009, 105 : 141 - 157
  • [48] Tracking control design for fractional order systems: A passivity-based port-Hamiltonian framework
    Kumar, Lalitesh
    Dhillon, Sukhwinder Singh
    ISA TRANSACTIONS, 2023, 138 : 1 - 9
  • [49] Conditions of reducing effect of J2 perturbation on formation flying
    Li, Huayi
    Qiang, Wenyi
    Zhang, Yingchun
    Li, Baohua
    2006 IMACS: MULTICONFERENCE ON COMPUTATIONAL ENGINEERING IN SYSTEMS APPLICATIONS, VOLS 1 AND 2, 2006, : 717 - +
  • [50] Position control via force feedback for a class of standard mechanical systems in the port-Hamiltonian framework
    Munoz-Arias, Mauricio
    Scherpen, Jacquelien M. A.
    Dirksz, Daniel A.
    2013 IEEE 52ND ANNUAL CONFERENCE ON DECISION AND CONTROL (CDC), 2013, : 1622 - 1627