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Planetary Probe Entry Atmosphere Estimation Using Synthetic Air Data System
This paper develops an atmospheric state estimator based on inertial acceleration and angular rate measurements combined with a vehicle aerodynamic model. The approach utilizes the navigation state of the vehicle to recast the vehicle aerodynamic model to be a function solely of the atmospheric stat...
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| Publicado no: | J Spacecr Rockets |
|---|---|
| Main Authors: | , |
| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
2017
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| Assuntos: | |
| Acesso em linha: | https://ncbi.nlm.nih.gov/pmc/articles/PMC7756964/ https://ncbi.nlm.nih.gov/pubmed/33363293 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.2514/1.A34115 |
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