Adaptive Fault Tolerant Attitude Control of a Nano-Satellite with Three Magnetorquers and One Reaction Wheel-Reference-Cited by-同舟云学术

Adaptive Fault Tolerant Attitude Control of a Nano-Satellite with Three Magnetorquers and One Reaction Wheel

Published:2022-01 Issue:1 Volume:35 Page:04021113
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sadigh Sevil M.¹^ORCID,Kashaninia Abdorreza²^ORCID,Dehghan Seyyed Mohammad Mehdi³^ORCID

Affiliation:

1. Ph.D. Student, Faculty of Electrical and Computer Engineering, Malek Ashtar Univ. of Technology, Lavizan, Tehran 15875-1774, Iran. ORCID: .

2. Assistant Professor, Faculty of Electrical and Computer Engineering, Malek Ashtar Univ. of Technology, Lavizan, Tehran 15875-1774, Iran (corresponding author). ORCID: .

3. Assistant Professor, Faculty of Electrical and Computer Engineering, Malek Ashtar Univ. of Technology, Lavizan, Tehran 15875-1774, Iran. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001321

Reference39 articles.

1. A fault-tolerant attitude tracking control of spacecraft using an anti-unwinding robust nonlinear disturbance observer

2. Attitude tracking with an adaptive sliding mode response to reaction wheel failure

3. Robust fault-tolerant tracking control design for spacecraft under control input saturation

4. Adaptive fault-tolerant spacecraft attitude control design with transient response control;Bustan D.;IEEE/ASME Trans. Mechatron.,2013

5. Improved Spacecraft Magnetic Attitude Maneuvering

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