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Showing 1 to 2 of 2 for “"Ascent Guidance"”.
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Ascent guidance for a winged boost vehicle
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.
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Pitch-Control Predictor-Corrector and Neural Network Ascent Guidance
A pitch-control predictor-corrector ascent guidance algorithm has been developed and evaluated for a rocket-based upper stage of a two-stage-to-orbit launch vehicle. Detailed descriptions of the predictor-corrector algorithm and a neural network loop modification are given. The mission requirement …