Trajectory control algorithms for the de-orbiting and Re-entry of the MISTRAL satellite-Reference-Cited by-同舟云学术

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Trajectory control algorithms for the de-orbiting and Re-entry of the MISTRAL satellite

Published:2023-02 Issue: Volume:203 Page:392-406
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Nocerino A.^ORCID,Notaro I.,Morani G.^ORCID,Poderico M.^ORCID,D'Amato E.,Blasi L.^ORCID,Fedele A.,Fortezza R.,Grassi M.^ORCID,Mattei M.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference87 articles.

1. The parashield entry vehicle concept: basic theory and flight test developments;Akin,1990

2. Inflatable Reentry and Descent Technology (Irdt) - Further Developments;Wilde,2001

3. Post-flight analysis of inflatable reentry and descent technology blackout during earth re-entry;Reynier;J. Spacecraft Rockets,2009

4. Inflatable re-entry technologies: flight demonstration and future prospects;Marraffa;ESA Bull.,2000

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1. Onboard generation of reentry trajectory for RLV via regularized extreme learning machine and marine predator whale optimizer;Advances in Space Research;2024-07

2. Inflatable aerodynamic decelerators for CubeSat reentry and recovery: Surface properties;Aerospace Science and Technology;2024-06

3. Incremental model predictive control for satellite de-orbiting based on drag modulation;Acta Astronautica;2024-02

4. Direct Adaptive Fuzzy Control with Prescribed Tracking Accuracy for Orbit Adjustment of Satellites;Actuators;2024-01-04

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