An explicit closed-loop guidance for launch vehicles

DOI10.1016/0094-5765(91)90139-VzbMath0723.70031OpenAlexW2074907194MaRDI QIDQ3210950

M. Seetharama Bhat, R. Vijaya Vittal

Publication date: 1991

Published in: Acta Astronautica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0094-5765(91)90139-v

zbMATH Keywords

inertial frameclosed-loop guidance logicEnke's methodexplicit, near optimal, closed-loop steering logicguided trajectorylaunch trajectories

Mathematics Subject Classification ID

Automated systems (robots, etc.) in control theory (93C85) Control of mechanical systems (70Q05) Kinematics of mechanisms and robots (70B15) Orbital mechanics (70M20)

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Guidance and control of a launch vehicle using a stochastic gradient projection method ⋮ Performance of parallel shooting method for closed loop guidance of an optimal launch vehicle trajectory

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