Event-Triggered Moving Horizon Pose Estimation for Spacecraft Systems

被引：0

作者：

Li S. ^{[1
]}

Zou H. ^{[2
]}

Shi D. ^{[1
]}

Wang J. ^{[1
]}

机构：

[1] School of Automation, Beijing Institute of Technology, Beijing

[2] China Academy of Space Technology, Beijing

来源：

Journal of Beijing Institute of Technology (English Edition) | 2022年 / 31卷 / 04期

关键词：

event-triggered; moving horizon estimation; pose estimation; state estimation;

D O I：

10.15918/j.jbit1004-0579.2022.008

中图分类号：

学科分类号：

摘要：

An event-triggered moving horizon estimation strategy is proposed for spacecraft pose estimation. The error dual quaternion is used to describe the system state and construct the spacecraft attitude-orbit coupled model. In order to reduce the energy consumption on spacecraft, an event-triggered moving horizon estimator (MHE) is designed for real-time pose estimation with limited communication resources. The model mismatch caused by event-triggered is finally solved by solving the cost function of the min-max optimization problem. The system simulation model is built in Matlab/Simulink, and the spacecraft pose estimation simulation is carried out. The numerical results demonstrate that the designed estimator could ensure the estimation effect and save spacecraft communication and computing resources effectively. © 2022 Beijing Institute of Technology. All rights reserved.

引用

页码：382 / 390

页数：8

共 15 条

[1]

Deng Y., Wang Z., Liu L., Unscented Kalman filter for spacecraft pose estimation using twistors, Journal of Guidance Control & Dynamics, 39, 8, pp. 1844-1856, (2016)

[2]

Choukroun D., Zivan Y., Vision-aided spacecraft relative pose estimation via dual quaternions, IEEE 58th Conference on Decision and Control, pp. 7893-7898, (2019)

[3]

Shi J., Ulrich S., Uncooperative spacecraft pose estimation using monocular monochromatic images, Journal of Spacecraft and Rockets, 58, 7, pp. 1-18, (2021)

[4]

Di F., Li A., Guo Y., Event-triggered sliding mode attitude coordinated control for spacecraft formation flying system with disturbances, Acta Astronautica, 188, 2, pp. 121-129, (2021)

[5]

Fan R., Chen X., Liu M., Attitude-orbit coupled sliding mode tracking control for spacecraft formation with event-triggered transmission, ISA Transactions, 124, 6, pp. 338-348, (2020)

[6]

Lefferts E. J., Markley F. L., Shuster M. D., Kalman filtering for spacecraft attitude estimation, Journal of Guidance Control Dynamics, 5, 5, pp. 536-542, (1982)

[7]

Lichten S. M., Border J. S., Strategies for high-precision global positioning system orbit determination, Journal of Geophysical Research Solid Earth, 92, B12, pp. 12751-12762, (1987)

[8]

Wang J., Research on integrated dynamic modeling, control and navigation methods of spacecraft attitude and orbit, (2013)

[9]

Sveier A., Egeland O., Pose estimation using dual quaternions and moving horizon estimation, 2nd IFAC Conference on Modelling, Identification and Control of Nonlinear Systems, pp. 186-191, (2018)

[10]

Filipe N., Kontitsis M., Tsiotras P., Extended Kalman filter for spacecraft pose estimation using dual quaternions, Journal of Guidance Control & Dynamics, 38, 9, pp. 1625-1641, (2015)

← 1 2 →