TECHNICAL NOTES - Effects of Flameholder Configuration on a Staged Supersonic Combustor
Tuning functions-based output feedback adaptive spacecraft formation flying despite disturbances
Effects of Fuel Injectors and Cavity Configurations on Supersonic Combustion
Noncertainty-Equivalent Adaptive Wing-Rock Control via Chebyshev Neural Network
Immersion- and invariance-based adaptive missile control using filtered signals
Variable-Structure Model Reference Adaptive Formation Control of Spacecraft
Study on the Suppression of Cavitation Instability in a Two-Stage Inducer
Noncertainty-Equivalent Adaptive Missile Control via Immersion and Invariance
Cavitation Performance and Instability of a Two-Bladed Inducer
Multi-Input Noncertainty-Equivalent Adaptive Control of an Aeroelastic System
Longitudinal Flight Dynamics of Bioinspired Ornithopter Considering Fluid-Structure Interaction
Numerical Analysis of Quasi-Steady-Combustion Characteristics in a Solid Rocket Motor
Real-Time Gaze Estimator Based on Driver's Head Orientation for Forward Collision Warning System
Control of plume interference effects on axisymmetric afterbodies
Geometric Characterization of Road Humps for Speed-Control Design. T. F. Fwa and L. S. Tan