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Stabilität
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18-Degree-of-Freedom Controller Design for the ST7 Disturbance Reduction System
50+ Years of NASA Mirror Technology Development: From Hubble to JWST and Beyond
50+ Years of NASA Mirror Technology Development: From Hubble to JWST and Beyond
50+ Years of NASA Mirror Technology Development: From Hubble to JWST and Beyond
150 kW Class Solar Electric Propulsion Spacecraft Power Architecture Model
757 NLF (Natural Laminar Flow) Glove Flight Test Results
1982 AFOSR/AFRPL Rocket Propulsion Research Meeting Held at Lancaster, California on 2-4 March 1982
1998 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 1 Part 2
1999 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 2 Part 1
2008 Stability, Security, Transition and Reconstruction Operations Conference
AAS/GSFC 13th International Symposium on Space Flight Dynamics, Volume 2
Abort Separation Study of a Shuttle Orbiter and External Tank at Hypersonic Speeds
A brief review of aircraft controls research opportunities in the general aviation field
A Brushless DC Torquer-Driven Reaction Wheel for Spacecraft Attitude Control
Absolute Stability Analysis of Attitude Control Systems for Large Boosters
A Calculation of the Lateral Hunting Motion of a Tracked Vehicle
A Calculation of the Profile Drag of Airfoils at Low Mach Numbers
Accident Avoidance Capabilities of Mopeds. Volume I: Executve Summary
Accident Avoidance Capabilities of Mopeds. Volume II: Technical Report
Accurate and Efficient Vortex-Capturing for Rotor Blade Vortex Interaction
Achieving Adequate United States Maritime Capital in an Era of Declining Resources
A Class of Selenocentric Retrograde Orbits With Innovative Applications to Human Lunar Operations
A Comment on a Critical Case of the Stability of a Singular Point on a Plane
A Comparison and Evaluation of Two Methods of Extracting Stability Derivatives from Flight Test Data
A Comparison of in-Flight and Ground Based Pitch Attitude Tracking Experiments
A comparison of some predicted and measured variables for a full-scale Surveyor drop test
A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model
A comparison of theory and experiment for aeroelastic stability of a hingeless rotor model in hover