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- W1479957899 abstract "The Aeroassist Flight Experiment scheduled for the early 1990's will demonstrate the use of a low L/D lifting brake using aerodynamic drag to return a spacecraft from a high energy to a low earth orbit. The experimental vehicle will be deployed and retrieved by the Shuttle Orbiter. This paper reviews some of the challenges, problems, and solutions encountered to date during guidance system development, with emphasis on technology advances which will benefit an operational Orbit Transfer Vehicle (OTV). Key factors to be discussed include guidance alternatives, aerodynamic modeling, navigation requirements, the impact of atmospheric uncertainties, and flight profile alternatives considered during initial planning." @default.
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- W1479957899 date "1986-01-01" @default.
- W1479957899 modified "2023-09-25" @default.
- W1479957899 title "Aeroassist flight experiment guidance, navigation and control" @default.
- W1479957899 hasPublicationYear "1986" @default.
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