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launch vehicle
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Closed-loop atmospheric ascent guidance based on finite element method
Abort recovery strategy for future vertical landing systems
Multi-phase and dual aero/propulsive rocket landing guidance using successive convex programming
Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion
An approach for space launch vehicle conceptual design and multi-attribute evaluation
Machine-Learning and Physics-Based Tool for Anomaly Identification in Propulsion Systems
Multidisciplinary design and optimization of expendable launch vehicle for microsatellite missions
Nonsingular terminal sliding mode control for reusable launch vehicle with atmospheric disturbances
Challenges in the development of a slow burning solid rocket booster
Strategic Forecasting Toward Achieving Defensible Space Architecture by Year 2030
An evaluation of the whole-spacecraft passive vibration isolation system
Reusable Launch of Small Satellites Using Scramjets
A new analytical model for reliability analysis of a launch vehicle system with limited test data
Unsteady Surface Pressure Characterization on Launch Vehicle in Liftoff Configuration
Conceptual study of a dual-rocket-based-combined-cycle powered two-stage-to-orbit launch vehicle
Hybrid optimization approach for rapid endo-atmospheric ascent trajectory planning
Ares V launch vehicle: An enabling capability for future space science missions
Ariane 5 Performance Optimization Using Dual-Bell Nozzle Extension
Evaluation of Exergy Efficiency Optimization of Space Launch Vehicles
Computational Assessment of the Efficiency of Using Various Fuel Pairs Onboard a Small Spacecraft
Impact of Geographical and Logistics Considerations on the Life Cycle Assessment of Launch Vehicles
Predefined-time control for a horizontal takeoff and horizontal landing reusable launch vehicle
Requirements Analysis of Propulsion Systems for Lunar-Exploration Mission
Retrofitting and Redesigning of Conventional Launch Systems for Small Satellites
Robust launch vehicle’s generalized dynamic inversion attitude control
Uncertainty Quantification of Artemis I Space Launch System Integrated Aerodynamics Databases
Issues and Perspectives on Space Launch Vehicles’ Development
An indirect adaptive predictive control for the pitch channel autopilot of a flight system
Comparison of Corcos-Based and Experimentally Derived Coherence Factors for Buffet Forcing Functions
Active Vibration Control of Launch Vehicle on Satellite Using Piezoelectric Stack Actuator
Modelling the Wall Pressure Fluctuations on the VEGA-C Launcher in Supersonic Conditions
The Aerospace Vehicle of the Future
Technologies of reducing the technological environmental impact of space rocket launches
Reviews and Challenges in Reliability Design of Long March Launcher Control Systems