Proportional-Integral-Type Event-Triggered Coupled Attitude and Orbit Tracking Control Using Dual Quaternions-Reference-Cited by-同舟云学术

Proportional-Integral-Type Event-Triggered Coupled Attitude and Orbit Tracking Control Using Dual Quaternions

Published:2022-08 Issue:4 Volume:58 Page:3021-3036
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Li Chunhui¹^ORCID,Zou Hengguang²,Shi Dawei¹^ORCID,Song Jiliang¹,Wang Junzheng¹^ORCID

Affiliation:

1. Authors’ addresses: State Key Laboratory of Intelligent Control and Decision of Complex Systems and School of Automation, Beijing Institute of Technology, Beijing, China

2. China Academy of Space Technology, Beijing, China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Link

http://xplorestaging.ieee.org/ielx7/7/9852357/09682588.pdf?arnumber=9682588

Reference43 articles.

1. ADRC based input disturbance rejection for minimum-phase plants with unknown orders and/or uncertain relative degrees

2. Event-triggered maximum likelihood state estimation

3. RodFIter: Attitude Reconstruction From Inertial Measurement by Functional Iteration

4. Rigid body motion tracking without linear and angular velocity feedback using dual quaternions

5. Coordinated control of relative position and attitude for spacecraft with actuator saturation

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