Angular Momentum Based Steering Approach for Control Moment Gyroscopes

被引：0
|
作者：
Geshnizjani, Ramin [1 ]
Kornienko, Andrei [2 ]
Fichter, Walter [1 ]
机构：
[1] Univ Stuttgart, Inst Flight Mech & Control, D-70569 Stuttgart, Germany
[2] Airbus DS GmbH, D-88039 Friedrichshafen, Germany
来源：
IFAC PAPERSONLINE | 2016年 / 49卷 / 17期
关键词：
Control moment gyroscopes; satellite control; steering laws; GYRO SYSTEMS;
D O I：
10.1016/j.ifacol.2016.09025
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
With increasing requirements on agile satellite missions, control moment gyroscopes (CMGs) become the actuator of choice due to their high torque amplification capability. In order to handle their inherent singularity issues, many steering laws have been developed that map a desired torque profile to a commanded gimbal rate profile. As CMGs are internal momentum exchange devices, alternative steering laws exist in the angular momentum/gimbal angle domain. In this paper, the two steering approaches are analyzed conceptually and their performance regarding the handling of singularities is evaluated in simulations. For a CMG array in roof configuration, the angular momentum/gimbal angle steering approach proves to be a viable choice for attitude control tasks. (C) 2016, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
引用
下载
收藏
页码：141 / 145
页数：5
相关论文
共 50 条
  • [21] Evaluation of Steering Algorithm Optimality for Single-Gimbal Control Moment Gyroscopes
    Leve, Frederick A.
    IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2014, 22 (03) : 1130 - 1134
  • [22] Simplified nonlinear control of attitude and momentum for space station using control moment gyroscopes
    Wu, Zhong
    Chou, W. S.
    DYNAMICS OF CONTINUOUS DISCRETE AND IMPULSIVE SYSTEMS-SERIES B-APPLICATIONS & ALGORITHMS, 2006, 13 : 236 - 240
  • [23] Global Singularity Avoidance Steering Law for Single-Gimbal Control Moment Gyroscopes
    Geng, Yunhai
    Hou, Zhili
    Huang, Simeng
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 40 (11) : 3034 - 3041
  • [24] Singularity analysis and steering law design for single-gimbal control moment gyroscopes
    Li C.-J.
    Guo Y.-N.
    Ma G.-F.
    Yuhang Xuebao/Journal of Astronautics, 2010, 31 (10): : 2346 - 2353
  • [25] Steering law design with perturbed Jacobian matrix for single gimbal control moment gyroscopes
    Wu, Zhong
    Wang, Zhen
    Deng, Shilong
    Yan, Ruidong
    2014 33RD CHINESE CONTROL CONFERENCE (CCC), 2014, : 2271 - 2275
  • [26] Steering Law Design to Control Moment Gyroscopes for Near Minimum Time Attitude Maneuver
    Guo, Yanning
    Ma, Guangfu
    Li, Chuanjiang
    ICIEA 2010: PROCEEDINGS OF THE 5TH IEEE CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS, VOL 1, 2010, : 301 - 306
  • [27] Angular-Momentum-Based Sizing of Control Moment Gyro Cluster for an Agile Spacecraft
    Mony, Abhilash
    Hablani, Hari B.
    Paranjape, Aditya A.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2022, 45 (09) : 1627 - 1643
  • [28] Feasible angular momentum of spacecraft installed with control moment gyros
    Leeghim, Henzeh
    Jin, Jaehyun
    Mok, Sung-Hoon
    ADVANCES IN SPACE RESEARCH, 2018, 61 (01) : 466 - 477
  • [29] Design and simulation of attitude control/momentum management system of space station using control moment gyroscopes
    School of Instrumentation, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
    Xitong Fangzhen Xuebao, 2006, 1 (151-154):
  • [30] Rapid Singularity-Escape Steering Strategy for Single-Gimbal Control Moment Gyroscopes
    Geng, Yunhai
    Hou, Zhili
    Guo, Jitang
    Huang, Simeng
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 40 (12) : 3199 - 3210
12345