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A Simple Control Scheme for the Problem of Spacecraft Transfer into a Target Orbit with Releasing the Separable Part of Its Launch Vehicle into the Earth’s Atmosphere

Crossref DOI link: https://doi.org/10.1134/S0010952524600562

Published Online: 2025-07-23

Published Print: 2025-06

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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