Discrete-Time Attitude Tracking Synchronization for Swarms of Spacecraft Exploiting Interference

被引：1
|
作者：
Li, Peiran [1 ]
Wen, Xin [1 ]
Zheng, Mohong [1 ]
Liu, Haiying [1 ,2 ]
Long, Dizhi [1 ]
Lu, Yuping [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Dept Astronaut, Nanjing 211100, Peoples R China
[2] Nanjing Ctr Appl Math, Nanjing 211135, Peoples R China
来源：
AEROSPACE | 2022年 / 9卷 / 03期
关键词：
aerospace; discrete event systems; nonlinear systems; synchronization; control over communications; EULER-LAGRANGE SYSTEMS; SUFFICIENT CONDITIONS; CONTAINMENT CONTROL; DIRECTED GRAPH; CONSENSUS; EIGENVALUE; MATRIX; DESIGN;
D O I：
10.3390/aerospace9030134
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The attitude tracking synchronization control of an orbit-predetermined leader-follower spacecraft swarm for the space moving target is discussed in this paper. The information exchange between all spacecraft is assumed to be discrete in time and on the undirected connected graph. Moreover, due to the demand for saving communication resources, wireless interference has been utilized, which allows all the neighbors of a spacecraft to access the same channel frequency spectrum simultaneously. Then the backstepping control algorithm is designed to let the spacecraft (beta,A)-practically stably synchronize their states and track a time-varying trajectory in the presence of unknown fading channels. Finally, simulation is provided to verify that using the proposed control scheme, the attitude tracking synchronization can be achieved with high precision.
引用
收藏
页数：24
相关论文
共 50 条
  • [1] Discrete-time Nonlinear Attitude Tracking Control of Spacecraft
    Ikeda, Yuichi
    2017 11TH ASIAN CONTROL CONFERENCE (ASCC), 2017, : 617 - 622
  • [2] Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference
    Peiran LI
    Xin WEN
    Haiying LIU
    Yuping LU
    Chinese Journal of Aeronautics , 2023, (02) : 241 - 255
  • [3] Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference
    LI, Peiran
    Wen, Xin
    Liu, Haiying
    Lu, Yuping
    CHINESE JOURNAL OF AERONAUTICS, 2023, 36 (02) : 241 - 255
  • [4] Event-triggered and consensus-based attitude tracking alignment for discrete-time multiple spacecraft system exploiting interference
    Peiran LI
    Xin WEN
    Haiying LIU
    Yuping LU
    Chinese Journal of Aeronautics, 2023, 36 (02) : 241 - 255
  • [5] Quaternion-based Discrete-time Nonlinear Attitude Tracking Control of Spacecraft
    Takaku, Yuichi
    Ikeda, Yuichi
    2020 AUSTRALIAN AND NEW ZEALAND CONTROL CONFERENCE (ANZCC 2020), 2020, : 75 - 80
  • [6] Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization
    Du, Haibo
    Li, Shihua
    Qian, Chunjiang
    IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2011, 56 (11) : 2711 - 2717
  • [7] Discrete-Time Optimal Attitude Control of a Spacecraft with Momentum and Control Constraints
    Phogat, Karmvir Singh
    Chatterjee, Debasish
    Banavar, Ravi
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2018, 41 (01) : 199 - 211
  • [8] Discrete-time low-computation spacecraft attitude tracking control algorithm design considering actuation stiff constraints
    Homaeinezhad, Mohammad Reza
    Nesaeian, Mahdi
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2024,
  • [9] Discrete-time 3-D Attitude Synchronization Based on Passivity Shortage
    Ibuki, Tatsuya
    Hatanaka, Takeshi
    Qu, Zhihua
    2018 IEEE CONFERENCE ON DECISION AND CONTROL (CDC), 2018, : 1293 - 1298
  • [10] Robust Tracking Control for A Type of Combined Spacecraft: A Discrete-Time FAS Approach
    Cui, Kai-Xin
    Duan, Guang-Ren
    2024 3RD CONFERENCE ON FULLY ACTUATED SYSTEM THEORY AND APPLICATIONS, FASTA 2024, 2024, : 1453 - 1458
12345