A suboptimal excitation torque for parameter estimation of a 5-DOF spacecraft simulator

被引:2
|
作者
Xu Zheyao [1 ,2 ]
Chen Yukun [3 ]
Xu Zhexuan [4 ]
机构
[1] Harbin Inst Technol, Sch Astronaut, Harbin 150001, Heilongjiang, Peoples R China
[2] Beijing Inst Astronaut Syst Engn, Beijing 100076, Peoples R China
[3] CASIC Space Engn Dev Co Ltd, Beijing 100039, Peoples R China
[4] Tianjin Univ, Tianjin 300072, Peoples R China
关键词
Parameter estimation; Spacecraft simulator; Excitation torque; ROBOT EXCITATION; TRAJECTORIES;
D O I
10.1016/j.asr.2018.07.029
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Five degrees of freedom spacecraft simulators are designed to verify spacecraft control strategies, rendezvous and docking techniques. The accurate knowledge of simulator inertia parameters which can be calculated by parameter estimation is of vital importance in these experiments. However, the rotation limits of the simulator must be considered during estimation process. This paper presents an approach to determine a suboptimal excitation torque for the system identification of the inertia parameters. The continuous optimization problem is transcribed into a discrete nonlinear programming problem by integral gauss pseudospectral method. To reduce the effect of noise, the states and inertia parameters are estimated simultaneously by joint filter within Extended Kalman Filter (EKF) or Unscented Kalman Filter (UKF). The proposed method is validated by simulations and the results indicate that this method not only satisfies the constraints of simulator rotation angles, but also improves the efficiency of parameter estimation. (C) 2018 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:2556 / 2565
页数:10
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