Conceptual Launch Vehicle and Spacecraft Design for Risk Assessment
Control-Oriented Aeroelastic Reduced-Order Modeling of Fighters
Methodologies for Predicting and Testing the Combat Damage on Flight Envelopes
Low-Cost Spacecraft Mission for Validating Formation Flying Technologies
Merged Vision and GPS Control of a Semi-Autonomous, Small Helicopter
Simulation-Based Analysis of Reentry Dynamics for the Sharp Atmospheric Entry Vehicle
Experiments in Aircraft Roll-Yaw Control using Forebody Tangential Blowing
Mars Micro-Meteorology Station Electronic Design, Assembly and Test Project
Aerodynamic Design of the Oblique Flying Wing Supersonic Transport
Vehicle Charging of the Shuttle Orbiter During Electron Beam Emission
Control of a Free-Flying Robot Manipulator System. Semiannual Report August 1985-February 1986