Unscented State Estimation for Rigid Body Attitude Motion with a Finite-time Stable Observer

被引:0
|
作者
Bohn, Jan J. [1 ]
Sanyal, Amit K. [2 ]
Butcher, Eric A. [3 ]
机构
[1] Raytheon Missile Syst, GNC Ctr, Tucson, AZ 85756 USA
[2] Syracuse Univ, Mech & Aerosp Engn, Syracuse, NY 13244 USA
[3] Univ Arizona, Mech & Aerosp Engn, Tucson, AZ 85721 USA
关键词
SPACECRAFT ATTITUDE; MODEL;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A discrete-time attitude state estimation scheme that uses a global representation of the configuration space for rigid body attitude motion, is presented. This estimation scheme uses discrete-time state measurements of inertially known vectors along with rate gyro measurements of the angular velocity, to obtain state estimates in the filtering stage. Additionally, a set of sigma points is obtained from the unscented transform based on exponential coordinates, with re-sampling centered at the current state estimate at each measurement instant. The state estimates along with sampled sigma points are propagated between measurement instants, using a discrete-time attitude state observer that is almost globally finite-time stable. The propagated sigma points and state estimate are enclosed by a minimum volume ellipsoid at the measurement instant. It is assumed that all states are measured at a constant measurement sample rate and that state measurement errors are bounded by an ellipsoidal bound. The update stage of the filter consists of finding the minimum volume enclosing ellipsoid that contains the propagated sigma points and the measurement uncertainty hound. This updated ellipsoid provides the filtered uncertainty bound and its center provides the updated state estimate. A new set of sigma points is selected from this ellipsoid and the propagation and update steps are repeated between measurement instants. Numerical simulation results confirm the analytically obtained stability properties of the attitude state observer. Numerical results also show that state estimate errors are bounded in the presence of bounded measurement noise and hounded disturbance torque.
引用
收藏
页码:4698 / 4703
页数:6
相关论文
共 50 条
  • [31] Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite
    Huo, Mingyi
    Huo, Xing
    Karimi, Hamid Reza
    Ni, Jianfei
    ABSTRACT AND APPLIED ANALYSIS, 2014,
  • [32] Almost global finite-time stabilization of rigid body attitude dynamics using rotation matrices
    Bohn, Jan
    Sanyal, Amit K.
    INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2016, 26 (09) : 2008 - 2022
  • [33] Finite-time angular velocity observers for rigid-body attitude tracking with bounded inputs
    Gui, Haichao
    Vukovich, George
    INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2017, 27 (01) : 15 - 38
  • [34] Continuous finite-time extended state observer based fault tolerant control for attitude stabilization
    Li, Bo
    Hu, Qinglei
    Yang, Yongsheng
    AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 84 : 204 - 213
  • [35] Finite-Time Control Algorithm Based on Modal State Observer for Flexible Satellite Attitude Tracking
    Li, Sijia
    Wu, Qiang
    IEEE ACCESS, 2020, 8 (08): : 184722 - 184730
  • [36] Velocity-Observer-Based Distributed Finite-Time Attitude Tracking Control for Multiple Uncertain Rigid Spacecraft
    Cui, Bing
    Xia, Yuanqing
    Liu, Kun
    Wang, Yujuan
    Zhai, Di-Hua
    IEEE TRANSACTIONS ON INDUSTRIAL INFORMATICS, 2020, 16 (04) : 2509 - 2519
  • [37] Landmark based nonlinear observer for rigid body attitude and position estimation
    Vasconcelos, J. F.
    Cunha, R.
    Silvestre, C.
    Oliveira, P.
    PROCEEDINGS OF THE 46TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-14, 2007, : 2506 - 2511
  • [38] Rigid Spacecraft Attitude Control Based on Finite-Time Non-Singular Sliding Mode and Extended State Disturbance Observer With Input Hysteresis
    Liu, Junjun
    Cui, Yufu
    Wang, Haoping
    Tian, Yang
    Zhou, Xingyu
    INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2025,
  • [39] Finite-Time Extended State Observer-Based Fixed-Time Attitude Control for Hypersonic Vehicles
    Zhao, Jiaqi
    Feng, Dongzhu
    Cui, Jiashan
    Wang, Xin
    MATHEMATICS, 2022, 10 (17)
  • [40] Finite-time stable disturbance observer for unmanned aerial vehicles
    Bhale, Pradhyumn
    Kumar, Mrinal
    Sanyal, Amit K.
    2022 AMERICAN CONTROL CONFERENCE, ACC, 2022, : 5010 - 5015