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Exhibit D modular design attitude control system study
Unconventional missile concepts from consideration of varied mission requirements
Minimum time slew of the SCOLE configuration
On-line determination of optimal flight paths for helicopters
Drop Tower Tests for Munitions
Fixed-Cone Valve Prototype Tests, Final Series, New Melones Dam, California
Auto vibration analysis combines CAT and CAE
Description of an experimental expert system flight status monitor
Newly developed spot test for evaluation of marine fuel stability
Feasibility study for ergonomic analysis and design of future helicopter cockpit systems
A simple microgravity table for the Orbiter or Space Station
Postflight evaluation of the solar maximum spacecraft magnetometers
Wisconsin Electric and Hybrid Vehicle Demonstration Project. Final Report, 1981-1985
Effect of Helicopter Vibration on the Accuracy of a Voice Recognition System
Air Force Technical Objective Document, Flight Dynamics Laboratory Plans for Fiscal Year 1988
Design sensitivity analysis for an aeroelastic optimization of a helicopter blade
Command and control of the Voyager spacecraft
Evaluation of on-line pulse control for vibration suppression in flexible spacecraft
Mariner Mark II - Spacecraft control for the 1990's and beyond
USEFUL LIFE DETERMINATION CHEMICAL OXYGEN GENERATORS
Space-Based Surveillance and Tracking System (SSTS), Environmental Assessment
Aircraft integrated design and analysis: A classroom experience
Aeroelastic optimization of a helicopter rotor
Combined problem of slew maneuver control and vibration suppression
An integrated automatic measuring system for internal ballistics testing
Movement measurements during flight tests of a missile
Analysis of Lateral-Directional Handling Qualities and Eigenstructure of High Performance Aircraft
Diagnostic testing of transformers on British Railways
Radiation testing of semiconductor devices for space electronics
Estimating time delay and transfer function parameters using wideband transient signals
Parallel dynamic programming for on-line flight path optimization
Delta II secondary payload opportunities for tether demonstration experiments