Quaternion-Based Hybrid Control for Robust Global Attitude Tracking

被引:292
|
作者
Mayhew, Christopher G. [1 ]
Sanfelice, Ricardo G. [2 ]
Teel, Andrew R. [3 ]
机构
[1] Robert Bosch Res & Technol Ctr, Palo Alto, CA 94304 USA
[2] Univ Arizona, Dept Aerosp & Mech Engn, Tucson, AZ 85721 USA
[3] Univ Calif Santa Barbara, Ctr Control Dynam Syst & Computat, Dept Elect & Comp Engn, Santa Barbara, CA 93106 USA
基金
美国国家科学基金会;
关键词
Attitude control; hybrid control; output feedback; robustness; spacecraft; RIGID-BODY; STABILIZATION; FEEDBACK; REJECTION; OBSERVER; DYNAMICS;
D O I
10.1109/TAC.2011.2108490
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
It is well known that controlling the attitude of a rigid body is subject to topological constraints. We illustrate, with examples, the problems that arise when using continuous and (memoryless) discontinuous quaternion-based state-feedback control laws for global attitude stabilization. We propose a quaternion-based hybrid feedback scheme that solves the global attitude tracking problem in three scenarios: full state measurements, only measurements of attitude, and measurements of attitude with angular velocity measurements corrupted by a constant bias. In each case, the hybrid feedback is dynamic and incorporates hysteresis-based switching using a single binary logic variable for each quaternion error state. When only attitude measurements are available or the angular rate is corrupted by a constant bias, the proposed controller is observer-based and incorporates an additional quaternion filter and bias observer. The hysteresis mechanism enables the proposed scheme to simultaneously avoid the "unwinding phenomenon" and sensitivity to arbitrarily small measurement noise that is present in discontinuous feedbacks. These properties are shown using a general framework for hybrid systems, and the results are demonstrated by simulation.
引用
收藏
页码:2555 / 2566
页数:12
相关论文
共 50 条
  • [21] Error quaternion-based spacecraft attitude tracking system with sliding mode control
    Feng, Lu
    Gong, Cheng
    He, Changan
    Yuhang Xuebao/Journal of Astronautics, 2000, 21 (01): : 17 - 22
  • [22] Quaternion-Based Indirect Adaptive Fuzzy Predictive Control for Attitude Tracking of Satellites
    Zhou, Yerong
    Huo, Wei
    2010 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-5, 2010, : 3087 - 3092
  • [23] On Quaternion-Based Attitude Control and the Unwinding Phenomenon
    Mayhew, Christopher G.
    Sanfelice, Ricardo G.
    Teel, Andrew R.
    2011 AMERICAN CONTROL CONFERENCE, 2011, : 299 - 304
  • [24] Quaternion-based Adaptive Terminal Sliding Mode Control for Spacecraft Attitude Tracking
    Wu, Shunan
    Wu, Guoqiang
    Tan, Shujun
    Wu, Zhigang
    2013 10TH IEEE INTERNATIONAL CONFERENCE ON CONTROL AND AUTOMATION (ICCA), 2013, : 913 - 917
  • [25] Quaternion-Based Direct Adaptive Fuzzy Predictive Control for Attitude Tracking of Satellites
    Zhou Ye-rong
    Huo Wei
    2009 IEEE INTERNATIONAL CONFERENCE ON INTELLIGENT COMPUTING AND INTELLIGENT SYSTEMS, PROCEEDINGS, VOL 2, 2009, : 510 - 516
  • [26] Quaternion-based Hybrid Feedback for Global Asymptotic Attitude Stabilization on S3
    Hashemi, Seyed Hamed
    Pariz, Naser
    Sani, Seyed Kamal Hosseini
    2021 7TH INTERNATIONAL CONFERENCE ON CONTROL, INSTRUMENTATION AND AUTOMATION (ICCIA), 2021, : 104 - 108
  • [27] Unit quaternion-based output feedback for the attitude tracking problem
    Tayebi, Abdelhamid
    IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2008, 53 (06) : 1516 - 1520
  • [28] Quaternion-based Finite-time Control for Attitude Tracking of the Spacecraft without Unwinding
    Guo, Yong
    Song, Shen-Min
    Li, Xue-Hui
    INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 2015, 13 (06) : 1351 - 1359
  • [29] Quaternion-based finite-time control for attitude tracking of the spacecraft without unwinding
    Yong Guo
    Shen-Min Song
    Xue-Hui Li
    International Journal of Control, Automation and Systems, 2015, 13 : 1351 - 1359
  • [30] The Quaternion-based Attitude Control System with an Augmented Dynamic
    Septanto, Harry
    Trilaksono, Bambang Riyanto
    Syaichu-Rohman, Arief
    Poetro, Ridanto Eko
    Ibrahim, Adrianto Ravi
    PROCEEDINGS OF 2013 3RD INTERNATIONAL CONFERENCE ON INSTRUMENTATION, COMMUNICATIONS, INFORMATION TECHNOLOGY, AND BIOMEDICAL ENGINEERING (ICICI-BME), 2013, : 190 - 193