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AC Current Ripple in Three-Phase Four-Leg PWM Converters with Neutral Line Inductor
A Pulse-Jet Control Method of Electromagnetic Projectiles Based on Impact Point Prediction
Prediction of DC-Link Voltage Switching Ripple in Three-Phase Four-Leg PWM Inverters
Hysteresis-Based Current Control Approach by Means of the Theory of Switched Systems
Hysteresis-Based Current Control Approach by Means of the Theory of Switched Systems
Safety-Enhanced Driver Condition Monitoring System for Preventing Road Accidents in Automobile
Wall Heat Loads in a Cryogenic Rocket Thrust Chamber During Thermoacoustic Instabilities
Unexpected Collision Detection, Estimation, and Reaction for a Free-Flying Orbital Robot
Acoustic Modes in a Plenum Downstream of a Multitube Pulse Detonation Combustor
20W Multi-output Isolated Power Supply Using Secondary Regulated Flyback Topology
Effects of Stick-Slip in Behavior of Structures with Friction Damper under Near-Field Earthquakes
Variable Frequency and Voltage Control of Induction Motor for Electric Vehicles
A Brief History of Laser Propulsion
Basic Gas-Dynamic Theories of the Laser Air-Breathing and Rocket Propulsion
Capabilities and limitations of existing hypersonic facilities
In-flight testing of the injection of the LISA Pathfinder test mass into a geodesic
Design and Modeling of an Impulse Continuously Variable Transmission with a Rotational Swashplate
Three-impulse point return orbit design for the manned lunar high-latitude exploration mission
An overview on the development of the U.S. navy full ship electromagnetic pulse simulators
Implementasi Fuzzy Logic Controller Pada Kendali Kecepatan Sepeda Bertenaga Angin
Fuzzy Logic Controller sebagai Penentu Gerak Mobile Robot Pembasmi Hama
Structural response and wall thickness design of pulse detonation combustor
Challenges in Design of Very High-Speed Data Acquisition System for High-Altitude Application
Design and Test of a Student Hybrid Rocket Engine with an External Carbon Fiber Composite Structure
Design and Test of a Student Hybrid Rocket Engine with an External Carbon Fiber Composite Structure
Jet thrust penetrators for sounding the surface layer of space bodies
Development of a Low-Latency Wireless Telemetry System for Monitoring Patients Heart Rates
Dynamic Features of Internal and External Flowfields of Pulsejet Engines
Minimum-Eigenvalue-Based Fault-Tolerant Adaptive Dynamic Control for Spacecraft
Static and Dynamic Behaviors of Basalt Fiber Reinforced Cement-Soil after Freeze-Thaw Cycle
Collision-Inclusive Trajectory Optimization for Free-Flying Spacecraft
Flow Characterization of Heavy-Lift Helicopter Rear Fuselage with Pulsed Jets for Separation Control
Frequency and Spark Timing Effects on Thrust for Pulse Detonation Engine
Gas Thermometry by Optical Emission Spectroscopy Enhanced with Probing Nanosecond Plasma Pulse
Continuous Open Access Special Issue "Aircraft Design": Number 2/2020