Coupling of Advanced Guidance and Robust Control for the Descent and Precise Landing of Reusable Launchers
This paper investigates the coupling of successive convex optimization guidance with robust structured <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msub><mi>H</mi><mo>∞</mo></msub&...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2024-11-01
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| Series: | Aerospace |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/11/11/914 |
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