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• W1835293015 abstract "A reduced-order method employing decomposition, based on time scale separation, of the 4-D state space in a 2-D slow manifold and a family of 2-D fast manifolds is shown to provide an excellent approximation to the full-order minimum-fuel ascent trajectory. Near-optimal guidance is obtained by tracking the reduced-order trajectory. The tracking problem is solved as regulation problems on the family of fast manifolds, using the exact linearization methodology from nonlinear geometric control theory. The validity of the overall guidance approach is indicated by simulation." @default.
• W1835293015 created "2016-06-24" @default.
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• W1835293015 date "1990-05-01" @default.
• W1835293015 modified "2023-09-23" @default.
• W1835293015 title "Aerospace Plane Guidance using Geometric Control Theory" @default.
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• W1835293015 doi "https://doi.org/10.23919/acc.1990.4791046" @default.
• W1835293015 hasPublicationYear "1990" @default.
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