Robust Fractional Order PDD Control of Spacecraft Rendezvous

被引:0
|
作者
Sarafnia, Niloofar [1 ]
Malekzadeh, Maryam [1 ]
Askari, Javad [2 ]
机构
[1] Univ Isfahan, Engn Dept, Esfahan, Iran
[2] Tech Univ Isfahan, Engn Dept, Esfahan, Iran
来源
2016 4TH RSI INTERNATIONAL CONFERENCE ON ROBOTICS AND MECHATRONICS (ICROM) | 2016年
关键词
Spacecraft Rendezvous; Robust Control; Fractional Order PDD Controller (FOPDD); Actuator Saturation; Particle Swarm Optimization (PSO); GAIN SCHEDULED CONTROL; SYSTEMS;
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
A robust Fractional Order PDD (FOPDD) controller is designed for a nonlinear spacecraft rendezvous subject to uncertain conditions considering actuator saturation. The controller is designed for the linear and decouples system. It is applied on nonlinear uncertain system in large maneuverings. In order to design the FOPDD controller, the specifications are calculated through the phase margins, sensibility function and robustness constraints. The controller parameters are obtained through Particle Swarm Optimization (PSO) due to high convergence speed, low computation, easy simulation and rapid response. The simulation results indicate the designed FOPDD controller can track the desired trajectory in the composite uncertain condition (considering constant, impulse and sinusoidal disturbance, parametric uncertainty and sensor noises). The FOPDD performance is compared with the classic PDD controller for nonlinear model. The simulation is based on the SPHERES project.
引用
收藏
页码:42 / 48
页数:7
相关论文
共 50 条
  • [41] Robust H∞ control of spacecraft rendezvous system with input saturation: A gain scheduled approach
    Huang, Yi
    Jia, Yingmin
    2018 ANNUAL AMERICAN CONTROL CONFERENCE (ACC), 2018, : 4243 - 4248
  • [42] Optimal Low-Thrust Trajectory Design and Robust Tracking Control for Spacecraft Rendezvous
    Zhang Song
    Hou Mingshan
    Wang Dong
    Zhou Tao
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 4885 - 4888
  • [43] Robust control for spacecraft rendezvous system with actuator unsymmetrical saturation: a gain scheduling approach
    Wang, Qian
    Xue, Anke
    INTERNATIONAL JOURNAL OF CONTROL, 2018, 91 (06) : 1241 - 1250
  • [44] Robust adaptive backstepping neural networks control for spacecraft rendezvous and docking with input saturation
    Xia, Kewei
    Huo, Wei
    ISA TRANSACTIONS, 2016, 62 : 249 - 257
  • [45] AN OPTIMAL CONTROL APPROACH TO ROBUST CONTROL OF NONLINEAR SPACECRAFT RENDEZVOUS SYSTEM WITH theta-D TECHNIQUE
    Gao, Xiangyu
    Teo, Kok Lay
    Duan, Guangren
    INTERNATIONAL JOURNAL OF INNOVATIVE COMPUTING INFORMATION AND CONTROL, 2013, 9 (05): : 2099 - 2110
  • [46] Robust adaptive terminal sliding mode control on SE(3) for autonomous spacecraft rendezvous and docking
    Daero Lee
    George Vukovich
    Nonlinear Dynamics, 2016, 83 : 2263 - 2279
  • [47] Output Tracking Control for Autonomous Spacecraft Rendezvous
    Yang, Xuebo
    Bo, Yuming
    Liu, Yurong
    Ji, Zhijian
    Gao, Huijun
    PROCEEDINGS OF THE 48TH IEEE CONFERENCE ON DECISION AND CONTROL, 2009 HELD JOINTLY WITH THE 2009 28TH CHINESE CONTROL CONFERENCE (CDC/CCC 2009), 2009, : 5227 - 5232
  • [48] Robust Adaptive Control for Spacecraft Rendezvous with Predefined-Time Prescribed Performance and Input Saturation
    Hao, Yong
    Lin, Zhixian
    Su, Ziyi
    Xiao, Yunfei
    Huang, Bing
    JOURNAL OF AEROSPACE ENGINEERING, 2022, 35 (01)
  • [49] Control for rendezvous and docking with a tumbling target spacecraft
    Hu, Yong
    Xu, Li-Jia
    Xie, Yong-Chun
    Yuhang Xuebao/Journal of Astronautics, 2015, 36 (01): : 47 - 57
  • [50] Robust adaptive terminal sliding mode control on SE(3) for autonomous spacecraft rendezvous and docking
    Lee, Daero
    Vukovich, George
    NONLINEAR DYNAMICS, 2016, 83 (04) : 2263 - 2279