Reusability Flight Experiment Guidance: Trajectory Correction After Ascent
This paper presents the design and implementation of a guidance algorithm for the re-entry vehicle ReFEx (Reusability Flight Experiment). This algorithm aims at correcting for the dispersion in position and velocity after separation from the launcher, by updating the trajectory. The need for this up...
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| Hlavní autoři: | , , |
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| Médium: | Artigo |
| Jazyk: | Inglês |
| Vydáno: |
MDPI AG
2025-09-01
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| Edice: | Aerospace |
| Témata: | |
| On-line přístup: | https://www.mdpi.com/2226-4310/12/9/838 |
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