Spatial approaches to moons from resonance relative to invariant manifolds
Spatial approaches to moons from resonance relative to invariant manifolds
Predictive Control Design for an Unmanned Aerial Vehicle
Evaluation of Heat Pipes in the Temperature Range of 450 to 700 K
Aerodynamic design optimization on unstructured meshes using the Navier-Stokes equations
Aerodynamic Design Optimization on Unstructured Meshes Using the Navier-Stokes Equations
F-22 Aeroelastic Design and Test Validation AIAA Paper 2007-1764 CD-ROM Number 7
Loop Heat Pipe Radiator Trade Study for the 300-550 K Temperature Range
An MDO approach to Control-Configured-Vehicle design
An MDO Approach to Control-Configured-Vehicle Design
Safety Enhancements Available by Converting MSG-2 Aircraft Maintenance Programs to MSG-3