Robust predictor-corrector guidance for aeroassisted orbital transfer

DOI10.2514/3.21755zbMath0873.70018OpenAlexW2092676062MaRDI QIDQ4717247

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Publication date: 15 January 1997

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.21755

zbMATH Keywords

numerical testsdispersion effectsoptimization theory

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (3)

Optimal trajectories for Earth-to-Mars flight ⋮ Prediction-based guidance algorithm for high-lift reentry vehicles ⋮ Optimal ascent trajectories and feasibility of next-generation orbital spacecraft

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