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Multiple stage satellite launch vehicle ascent optimization using Chebyshev wavelets
Load relief control of launch vehicle using aerodynamic angle estimation
Re-entry trajectory optimization using an hp-adaptive Radau pseudospectral method
Global and robust attitude control of a launch vehicle in exoatmospheric flight
Adaptive control design for active Pogo suppression of large strap-on liquid launch vehicles
Advanced GNC-oriented modeling and simulation of Vertical Landing vehicles with fuel slosh dynamics
Generalization and transfer of advanced Ukrainian expertise in dynamic aerospace design to students
A study on metallic thermal protection system panel for Reusable Launch Vehicle
Aerospace launch vehicle control: an intelligent adaptive approach
Optimal tuning of adaptive augmenting controller for launch vehicles in atmospheric flight
The Space Launch Services Industry: Indicators and Trends
New multidisciplinary design optimization approaches for launch vehicle design
Satellite Launch and In‐orbit Operations
A novel metamodel management strategy for robust trajectory design of an expendable launch vehicle
Stability analysis of explicit guidance laws for space launch vehicles with varying thrust integrals
Design of Synthetic Diagnostic and Health Management of Launch Vehicle
Improvement of UAV: design and implementation on launchability
A reliable analytical navigation system based on symmetrical dynamic behavior of control channels
Switching robust control for a nanosatellite launch vehicle
Launch Vehicle Health Management
Vector Field-based Guidance Development for Launch Vehicle Re-entry via Actuated Parafoil
Longitudinal control of an aerospace launch vehicle: a backstepping approach
A review of UK space activity and historiography, 1957–2007
Assessment and development of a ROM for linearized aeroelastic analyses of aerospace vehicles
A comparison of iterative explicit guidance algorithms for space launch vehicles
Launch Vehicle Ascent Computational Fluid Dynamics for the Space Launch System
Lumped parameter modelling for the thermal analysis of the launch vehicle Vega C
Closed-loop atmospheric ascent guidance based on finite element method