Rendezvous Missions to Systems of Small Solar System Bodies Using the Suboptimal SDRE Control Approach

Rendezvous Missions to Systems of Small Solar System Bodies Using the Suboptimal SDRE Control Approach

In this work, we analyze the suitability of the State-Dependent Riccati Equation (SDRE) suboptimal nonlinear control formulation for the implementation of body-fixed hovering of a spacecraft in the highly nonlinear environment engendered by the faint force fields around single- and multi-body Near-E...

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Bibliographic Details
Main Authors: Edson Cereja, José Manoel Balthazar, Angelo Marcelo Tusset, Vladimir Razoumny, Antonio Fernando Bertachini de Almeida Prado
Format: Article
Language:English
Published: MDPI AG 2025-02-01
Series:Applied Sciences
Subjects:
small solar system bodies
Near-Earth Objects
asteroid system
ASTER mission
body-fixed hovering
nonlinear control
Online Access:https://www.mdpi.com/2076-3417/15/4/1799
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