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The integration of scientific instruments into Mariner IV.
The integration of scientific instruments into mariner iv.
Nonlinear Aerodynamics of Bodies in Coning Motion
Spacecraft attitude control for a solar electric geosynchronous transfer mission
Dynamics of incremental motion devices associated with planetary exploration spacecraft
Aircraft energy efficiency laminar flow control glove flight conceptual design study
Pointing control for the International Comet Mission
Interactive design and analysis of future large spacecraft concepts
Type 'A' V/STOL - One aircraft for all support missions
Autonomous spacecraft maintenance study group
Multiwall TPS: An emerging concept
Orbital Maneuvering Vehicle Simulation System On-Board Processing Logic
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
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
Description of an experimental expert system flight status monitor
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
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
Aircraft integrated design and analysis: A classroom experience
Aeroelastic optimization of a helicopter rotor
Combined problem of slew maneuver control and vibration suppression
Parallel dynamic programming for on-line flight path optimization
Delta II secondary payload opportunities for tether demonstration experiments
Recent Advances in Multidisciplinary Analysis and Optimization, part 1
Approach to transaction management for Space Station Freedom
Optimal decentralized feedback control for a truss structure
Initial flight qualification and operational maintenance of X-29A flight software
The DELTA MONSTER: An RPV designed to investigate the aerodynamics of a delta wing platform
STS payload design load evolution
Recent Advances in Multidisciplinary Analysis and Optimization, part 2
Aeroelastic modeling for the FIT (Functional Integration Technology) team F/A-18 simulation
Experiments in multivariable adaptive control of a large flexible structure