Optimal Attitude Control is a control strategy within the field of aerospace engineering that belongs to the class of attitude control methods and is distinguished by its systematic minimization of a prescribed performance index, such as energy consumption or tracking error, while achieving precise orientation of a spacecraft or aircraft under dynamic constraints.
215
Publications
8.7K
Citations
485
Authors
190
Institutions
Publications per year
2017–2026
79
Parents
Publications
215
Runqi Chai, Antonios Tsourdos, Al Savvaris et al. · IEEE Transactions on Neural Networks and Learning Systems · 2019 · 177 citations · Full text
Engineering, Aerospace Engineering, Artificial Intelligence +14
1–5 of 215
Authors
485
- JL
7
h-index
- NH
5
h-index
- CY
5
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- ML
5
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- QH
5
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1–5 of 485
Institutions
190
Harbin Institute of Technology
Harbin, China
12 h-index
30 publications
1K citations
Beihang University
Beijing, China
12 h-index
31 publications
1K citations
Beijing Institute of Technology
Beijing, China
8 h-index
19 publications
1.6K citations
Virginia Tech
Blacksburg, United States
7 h-index
15 publications
421 citations
University of Michigan
Ann Arbor, United States
7 h-index
16 publications
620 citations
Indian Institute of Technology Kanpur
Kanpur, India
6 h-index
14 publications
574 citations
Nanjing University of Aeronautics and Astronautics
Nanjing, China
6 h-index
19 publications
340 citations
University of Toronto
Toronto, Canada
5 h-index
9 publications
180 citations
1–8 of 190
Venues
- Journal of Guidance Control and Dynamics
42 publications · 1.8K citations
23
h-index
- Aerospace Science and Technology
AST · 20 publications · 773 citations
17
h-index
- IEEE Transactions on Aerospace and Electronic Systems
12 publications · 564 citations
11
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- Acta Astronautica
11 publications · 306 citations
10
h-index
- IEEE Transactions on Automatic Control
6 publications · 157 citations
6
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1–5