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MISTRAL: Air-Launchable Micro-Satellite with Re-Entry Capability
A Hybrid Formulation for Modelling Multibody Spacecraft
Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle
Renato Koch: a protagonist of Electronics in the Nineteen hundreds
Development of finite element model for morphing inflatable winglet
General Methodology For Demonstration Mission Design
IDINTOS: the first prototype of an amphibious PrandtlPlane-shaped aircraft
Small whirlwind design semi-analytic model
Lares Mission: Engineering Aspects
Large Debris Removal Mission in LEO based on Hybrid Propulsion
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze Thin Walled Structures
Soviet Union Spacecraft that Explored Venus 1980–1990
Japanese and European Space Agency Spacecraft that Explored Venus 2005–2020
U.S. Magellan Spacecraft that Explored Venus 1980–2020
Model of Launch Vehicle Dynamics and Redundant Strapdown IMUs
Launch Vehicles for Planetary Spacecraft
Multistage Rocket Trajectory Re-planning
Optimal Control Problems and Common Solutions
A methodology for the identification of inertial properties of small size UAVs
A Tool for the Simulation of All-Electric Aircraft Systems
Soviet Union Spacecraft That Explored Venus 1960–1980
Wind Shear On-Line Identification for Unmanned Aerial Systems
Brushless Dc Motors Failure Detection Using The Continuous Wavelet Transform
Turbojet Steady State and Transient Analytical Model Development and Validation
U.S. Spacecraft that Explored Venus 1960–1980
USV3 System Concept Development Overview
Fatigue crack growth failure and lifing analyses for metallic aircraft structures and components
A non-linear model for in-plane shear damage and failure of composite laminates
Philae Attitude Determination through Nonlinear Optimal Identification of Solar Arrays Telemetry
Aircraft Damage Pattern Recognition Using Aerodynamic Coefficients and Fuzzy Logic
Robust Incremental Nonlinear Dynamic Inversion Controller of Hexapod Flight Simulator Motion System
Characterising Angular Accelerometer Calibration Setup Disturbance Using Box–Jenkins Method
A Space-Borne GNSS Receiver for Evaluation of the LEO Navigation Based on Real-Time Platform
Trajectory Shaping Guidance Law Based on Downrange-to-Go Polynomial
UAV Control System Reconfiguration Under Physical Constrains
Circumnavigation with Side-Bearing Angle
nxControl: Ground Mode for Manual Flight Control Laws with Longitudinal Load Factor Command
Comparison of Multiple Spacecraft Configuration Designs for Coordinated Flight Missions
Nonlinear Modular 3D Trajectory Control of a General Aviation Aircraft
Mechanical/Control Integrated Design of a Flexible Planar Rotatory Spacecraft