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- W94018542 abstract "Abstract The atmospheric flight of a spacecraft is considered when a aeroassisted orbit change maneuver is performed. Both guidance and control problems are solved and make respectively use of nonlinear control theory and classical adaptive control schemes. The originality of the work lies in the consideration of the overall guidance and control problem. A second point which is worth to be noticed is that focus is set on computational time. Whereas gain scheduling is known to be compatible with limited computing power, the main stream in literature consists in implementing some optimizing routines when the guidance problem is tackled. This scheme is dramatically time consuming and is deliberately skipped in the paper; it is replaced by a trajectory tracking guidance policy issued from modem nonlinear control theory. The guidance and control solution is shown to be quite unsensitive to atmospheric density deviations which constitute major unknown parameters in the higher layers of the atmosphere." @default.
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- W94018542 date "1992-09-01" @default.
- W94018542 modified "2023-09-23" @default.
- W94018542 title "Online Guidance and Control of a Spacecraft for an Aeroassisted Orbit Transfer" @default.
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- W94018542 doi "https://doi.org/10.1016/s1474-6670(17)49643-1" @default.
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