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ELECTROHYDRAULIC FLOW-CONTROL SERVOVALVES
The integration of scientific instruments into mariner iv.
The integration of scientific instruments into Mariner IV.
ELECTROHYDRAULIC FLOW-CONTROL SERVOVALVES
ELECTROHYDRAULIC FLOW-CONTROL SERVOVALVES
Spacecraft attitude control for a solar electric geosynchronous transfer mission
Dynamics of incremental motion devices associated with planetary exploration spacecraft
Interactive design and analysis of future large spacecraft concepts
Type 'A' V/STOL - One aircraft for all support missions
Multiwall TPS: An emerging concept
INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES
Interactive systems design and synthesis of future spacecraft concepts
Performance testing of the Galileo attitude control system
Aeroelastic model helicopter rotor testing in the Langley TDT
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
Description of an experimental expert system flight status monitor
Newly developed spot test for evaluation of marine fuel stability
Postflight evaluation of the solar maximum spacecraft magnetometers
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
Aircraft integrated design and analysis: A classroom experience
Aeroelastic optimization of a helicopter rotor
Combined problem of slew maneuver control and vibration suppression
Diagnostic testing of transformers on British Railways
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
Approach to transaction management for Space Station Freedom
Optimal decentralized feedback control for a truss structure
STS payload design load evolution
Aeroelastic modeling for the FIT (Functional Integration Technology) team F/A-18 simulation
Experiments in multivariable adaptive control of a large flexible structure
Pulse modulated control synthesis for a flexible spacecraft
Cost effective vibration testing for automotive electronics
Conversion of the PACE1750A CMOS chip set to silicon on sapphire (for military equipment)
CHEMICAL METHODS FOR THE MEASUREMENT OF NONREGULATED DIESEL EMISSIONS
A 150-MHz 1.25 mu m CMOS/SOS DSP integrated circuit
A method for optimal actuator and sensor placement for large flexible structures