Closed-loop Trajectory Guidance
Closed-Loop Trajectory Guidance is a launch vehicle trajectory guidance method that continuously adjusts the vehicle's flight path in real time by feeding measured state variables into a guidance algorithm to minimize deviations from the desired trajectory.
67
Publications
2.5K
Citations
171
Authors
71
Institutions
Publications per year
2017–2026
17
67
Rapid Optimal Multiburn Ascent Planning and Guidance
Ping Lu, Brian Griffin, Gregory A. Dukeman et al. · Journal of Guidance Control and Dynamics · 2008 · 108 citations
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71

Beijing Institute of Technology
Beijing, China
5 h-index
15 publications
636 citations
Iowa State University
Ames, United States
5 h-index
9 publications
681 citations

Harbin Institute of Technology
Harbin, China
4 h-index
12 publications
580 citations
Technion – Israel Institute of Technology
Haifa, Israel
3 h-index
5 publications
192 citations

Beihang University
Beijing, China
3 h-index
7 publications
210 citations
Jet Propulsion Laboratory
Pasadena, United States
3 h-index
8 publications
126 citations

Nankai University
Tianjin, China
2 h-index
5 publications
428 citations
Georgia Institute of Technology
Atlanta, United States
2 h-index
5 publications
187 citations
1–8 of 71
14 publications · 830 citations
14
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AST · 7 publications · 338 citations
7
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5 publications · 125 citations
5
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3 publications · 207 citations
3
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Conference · 3 publications · 42 citations
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