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- W3014785139 abstract "This paper describes a real-time abort guidance algorithm which determines the time sequence of the powered maneuvers and the orientation of the thrust vector throughout an abort-mission action initiated during the orbiter ascent phase. It involves guiding a heavily loaded Space Shuttle vehicle, passing through severe environmental conditions, back to a designated landing area. A graphical example and estimates of the computer requirements are included." @default.
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- W3014785139 date "1975-07-01" @default.
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- W3014785139 title "Real-time orbiter abort guidance" @default.
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