Application of L~1 Adaptive Control to a High Maneuverability Aircraft
ENGINEERING NOTES - Jump Markovian-Based Control of Wing Deployment for an Uncrewed Air Vehicle
An H~∞ Design Approach for a PID Automatic Flight Control System of a Launch Vehicle
Well-Conditioned Procedures for Optimal Robust Design of Flight Control Systems
An H~∞ Design Approach for the Heading Hold Autopilot of a Flying Wing UAV
Matching bent crystals to high-brilliance sources [3767-51]
Efficient Error Correcting Codes for On-Chip DRAM Applications for Space Missions
Attitude Control for Small Satellites Using Rotation Angles (IAA-AAS-DyCoSS1-07-06 - AAS 12-348)