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Aerodynamic Test and Analysis of a Slender Generic Missile Configuration
Postlanding optimum designs for the assured crew return vehicle
A method for optimal actuator and sensor placement for large flexible structures
Simulated rotor test apparatus dynamic characteristics in the 80- by 120-foot wind tunnel
Dynamics and control of tethered spacecraft - A brief overview
Component model reduction via the projection and assembly method
Hot-bench simulation of the active flexible wing wind-tunnel model
Space Station Simulation Computer System (SCS) study for NASA/MSFC. Concept document
The importance of batteries in unmanned missions
International Used Ship Market as a Temporary Solution to U.S. Sealift Requirements
Volume IV. Flight Test Management. Chapter 3. Systems/Test Safety
JANNAF Propulsion Meeting Held in Anaheim, California on 3-5 October 1990. Volume 2
Development of Ballistic Missiles in the United States Air Force, 1945-1960
Structural behavior of scientific balloons - Finite element simulation and verification
Singular control in minimum time spacecraft reorientation
An aircraft model for the AIAA controls design challenge
Experimental results of active control on a large structure to suppress vibration
Motion requirements for antennas in geostationary earth orbit
Identification and simulation evaluation of an AH-64 helicopter hover math model
Sensitivity of Space Station Alpha Joint robust controller to structural modal parameter variations
A fuzzy logic based spacecraft controller for six degree of freedom control and performance results
The Guardian: Preliminary design of a close air support aircraft
Volume 1. Performance Flight Testing. Annex 6A. Programmed Text for Supersonic Aerodynamics
Volume IV. Test Management Phase. Chapter 4. Logistics Flight Testing
Manned Flight Simulator and the Impact on Navy Weapons Systems Acquisition
Investigation of Airfield Runways at Jacksonville Naval Air Station
Use of Piloted Simulation for High-Angle-of-Attack Agility Research and Design Criteria Development
Testing and Evaluation of the Percussionaire Corporation Military Transporter Respirator, Model TXP
A three-frequency scatterometer technique for the measurement of ocean wave spectra
Multidisciplinary design integration system for a supersonic transport aircraft
Dynamics of spacecraft with deploying flexible appendages
Recent advances in integrated multidisciplinary optimization of rotorcraft
On-line analysis capabilities developed to support the AFW wind-tunnel tests
Extracting dimensional geometric parameters from B-spline surface models of aircraft
Structural Tailoring/Analysis for Hypersonic Components - A computational simulation
Preliminary design of a high speed civil transport: The Opus 0-001