Output-Constrained Attitude Tracking Control for Spacecraft with Adaptive Inertia and Disturbance Identifications-Reference-Cited by-同舟云学术

Output-Constrained Attitude Tracking Control for Spacecraft with Adaptive Inertia and Disturbance Identifications

Published:2023-09 Issue:5 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yao Qijia¹^ORCID,Li Qing²,Huang Chen³,Jahanshahi Hadi⁴

Affiliation:

1. Associate Professor, School of Automation and Electrical Engineering, Key Laboratory of Knowledge Automation for Industrial Processes of Ministry of Education, Univ. of Science and Technology Beijing, Beijing 100083, China. ORCID: .

2. Professor, School of Automation and Electrical Engineering, Key Laboratory of Knowledge Automation for Industrial Processes of Ministry of Education, Univ. of Science and Technology Beijing, Beijing 100083, China (corresponding author).

3. Graduate Student, School of Automation and Electrical Engineering, Univ. of Science and Technology Beijing, Beijing 100083, China.

4. Researcher, Dept. of Mechanical Engineering, Univ. of Manitoba, Winnipeg, MB, Canada R3T 5V6.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4984

Reference61 articles.

1. Adaptive Asymptotic Tracking of Spacecraft Attitude Motion with Inertia Matrix Identification

2. Backstepping Control Design with Actuator Torque Bound for Spacecraft Attitude Maneuver

3. Robust Adaptive Control of Feedback Linearizable MIMO Nonlinear Systems With Prescribed Performance

4. Adaptive Fault-Tolerant Spacecraft Attitude Control Design With Transient Response Control

5. Neural-Network-Based Adaptive Backstepping Control With Application to Spacecraft Attitude Regulation