Fault-Tolerant Model-Free Predictive Control of Spacecraft Coupled Rotational–Translational Relative Motion-Reference-Cited by-同舟云学术

Fault-Tolerant Model-Free Predictive Control of Spacecraft Coupled Rotational–Translational Relative Motion

Published:2021-11 Issue:6 Volume:34 Page:04021092
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Chiniforoushan Mohammad¹^ORCID,Raissi Kamran²,Mortazavi Mahdi³

Affiliation:

1. Ph.D. Candidate, Dept. of Aerospace Engineering, Amirkabir Univ. of Technology, Tehran 158754413, Iran. ORCID: .

2. Assistant Professor, Dept. of Aerospace Engineering, Amirkabir Univ. of Technology, Tehran 158754413, Iran (corresponding author).

3. Associate Professor, Dept. of Mechanical Engineering, Faculty of Engineering, Univ. of Isfahan, Isfahan 8174673441, Iran.

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.1943-5525.0001327

Reference74 articles.

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3. Nonlinear Model Predictive Control with Enhanced Actuator Model for Multi-Rotor Aerial Vehicles with Generic Designs

4. Blanke, M., M. Kinnaert, J. Lunze, and M. Staroswiecki. 2006. Diagnosis and fault-tolerant control. Berlin: Springer.

5. Spacecraft alignment determination and control for dual spacecraft precision formation flying

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