Rocket landing guidance using convex optimization and proportional navigation considering performance-limited engine
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Published:2022-12
Issue:
Volume:201
Page:209-223
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ISSN:0094-5765
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Container-title:Acta Astronautica
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language:en
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Short-container-title:Acta Astronautica
Author:
Xiong Fenfen,
Li ChaoORCID,
Zhao YueORCID,
Hu Xiao
Subject
Aerospace Engineering
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5. Attitude control of an underactuated spacecraft using quaternion feedback regulator and tube-based MPC;Mirshams;Acta Astronaut.,2017
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