Design for robustness using the -synthesis applied to launcher attitude and vibration control
Developing of Guidance and Control System for Enhanced Epsilon Launch Vehicle (AIAA 2016-2638)
SUPPORT STRUCTURE OF FIBER-REINFORCED RESIN HOLLOW BODY
Post-Flight Analysis of Hayabusa; Asteroid Sample Return Capsule (AAS 12-579)
Influence of Elastic Deformation on Unsteady Multi-Body Separation (AAS 12-571)