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launch vehicle
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Closed-loop atmospheric ascent guidance based on finite element method
Hybrid optimization approach for rapid endo-atmospheric ascent trajectory planning
Robust launch vehicle’s generalized dynamic inversion attitude control
Lumped parameter modelling for the thermal analysis of the launch vehicle Vega C
Multidisciplinary design and optimization of expendable launch vehicle for microsatellite missions
Predefined-time control for a horizontal takeoff and horizontal landing reusable launch vehicle
Improvement of UAV: design and implementation on launchability