System Critical Design Audit (CDA), Books 1, 2 and 3
Description of and Preliminary Tests Results for the Joint Damping Experiment (JDX)
Low-Mass Inflation Systems for Inflatable Structures
Reusable Launch Vehicle: Technology Development and Test Program
Spacecraft Jitter Attenuation Using Embedded Piezoelectric Actuators
STS-71 Shuttle/MIR Mission Report
Cassini RTG Program. Monthly technical progress report, October 2--October 29, 1995
Reusable Launch Vehicle Technology Program and the X-33 Advanced Technology Demonstrator
Control of Complex Multibody Spacecraft
Control of Complex Multibody Spacecraft
Study of the Space Station Freedom Response to the Disturbance Environment
Baseline Tests of an Autonomous Telerobotic System for Assembly of Space Truss Structures
Technology for Small Spacecraft
MSAT Boom Joint Testing and Load Absorber Design
Development of an all-composite spacecraft bus for small satellite programs
Control of Satellites with Microgravity Constraints: The COMET Control System
Overview of Recent Advances in System Identification
ASI's Space Automation and Robotics Programs: The Second Step
Definition of Ground Test for Verification of Large Space Structure Control
Analysis of the Loads Applied to a Heavy Space Station Rack During Translation and Rotation Tasks
Third International Symposium on Artificial Intelligence, Robotics, and Automation for Space 1994
Analytical Investigation of the Dynamics of Tethered Constellations in Earth Orbit, Phase 2
Launch System Design for Access to Space
NPS State Vector Analysis and Relative Motion Plotting Software for STS-51
Activities of the Center for Space Construction
Space Station Redesign Option A: Modular Buildup Concept
Heisei 3 Nendo HOPE Gainen Sekkei (Concept Study of the Space Transportation System HOPE in FY 1991)
Stanford Aerospace Research Laboratory Research Overview
Space Station Common Berthing Mechanism, a Multi-Body Simulation Application
Hypersonic Airbreathing Reusable Advanced Launcher: A Feasibility Study
Attitude Stabilization of a Rigid Spacecraft Using Gas Jet Actuators Operating in a Failure Mode
Extended Duration Lunar Lander
LSS Systems Planning and Performance Program
Satellite Attack Warning and Assessment Flight Experiment (SAWAFE)
Proceedings of the Fifth NASA/NSF/DOD Workshop on Aerospace Computational Control
Development of a Non-Linear Simulation for Generic Hypersonic Vehicles - ASUHS1
Multidisciplinary Aeroelastic Analysis of a Generic Hypersonic Vehicle
Prototype Space Fabrication Platform
Aerodynamic Flight Control to Increase Payload Capability of Future Launch Vehicles
Progress in Multidisciplinary Design Optimization at NASA Langley
On-Orbit Servicing for USAF Space Missions: A Phased Development Approach
Aerothermoelastic Analysis of a NASP Demonstrator Model