AIAA Scitech 2019 Forum 2019
DOI: 10.2514/6.2019-0430
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Model Fidelity Studies for Rapid Trajectory Optimization

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Cited by 4 publications
(1 citation statement)
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“…Control, guidance, and navigation of hypersonic vehicles is a challenging problem and active research area due to complex nonlinear physics and fast time scales. We demonstrate the utility of our proposed method to control a three degree of freedom point-mass model of a hypersonic glide vehicle using an aerodynamic surrogate model trained on data from the NASA X43 flight tests [12,[14][15][16].…”
Section: X43 Trajectory Controlmentioning
confidence: 99%
“…Control, guidance, and navigation of hypersonic vehicles is a challenging problem and active research area due to complex nonlinear physics and fast time scales. We demonstrate the utility of our proposed method to control a three degree of freedom point-mass model of a hypersonic glide vehicle using an aerodynamic surrogate model trained on data from the NASA X43 flight tests [12,[14][15][16].…”
Section: X43 Trajectory Controlmentioning
confidence: 99%