Large-angle Slew Dynamics
Large-Angle Slew Dynamics is a computational model in attitude-orbit coupling that characterizes the nonlinear rotational motion of spacecraft during reorientation maneuvers exceeding 90 degrees, distinguishing itself from small-angle approximations by explicitly accounting for inertial, gyroscopic, and orbital perturbation effects across full-range attitude transitions.
18
Publications
618
Citations
40
Authors
19
Institutions
Publications per year
2017–2026
1
Parents
18
Nonlinear Predictive Control of Spacecraft
John L. Crassidis, F. Landis Markley, Tobin Anthony et al. · Journal of Guidance Control and Dynamics · 1997 · 49 citations
1–5 of 18
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19
Lockheed Martin (United States)
Bethesda, United States
2 h-index
3 publications
112 citations
University of Michigan
Ann Arbor, United States
2 h-index
6 publications
591 citations
University of Nevada, Las Vegas
Las Vegas, United States
2 h-index
3 publications
105 citations

Delft University of Technology
Delft, The Netherlands
1 h-index
2 publications
36 citations
Goddard Space Flight Center
Greenbelt, United States
1 h-index
3 publications
147 citations

United States Naval Research Laboratory
Washington, United States
1 h-index
3 publications
120 citations
University of Nevada, Reno
Reno, United States
1 h-index
1 publications
73 citations
University of America
Murrieta, United States
1 h-index
1 publications
49 citations
1–8 of 19
6 publications · 375 citations
6
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2 publications · 32 citations
2
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1 publications · 16 citations
1
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1 publications · 20 citations
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AST · 1 publications · 15 citations
1
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1–5