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ATTITUDE
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Publications of Goddard Space Flight Center, 1963. Volume II - Space Technology
Analytical Methods for Resistance Jet Design Supplementary Report No. 1
Star Reference System and Occultation Problems
Preliminary Study of Inertial Guidance Laws
The Use of Integral Compensation in the Reaction Wheel Control Loop
Magnetic Fields - Reasons for Simulation and Methods Available
Research on the Design of Adaptive Control Systems, Volume 2 Final Report
An Automatic Attitude Control System for a Spinning Satellite - a Theoretical Assessment
Attitude Perturbations and Magnetic Control of a Spin-Stabilized Satellite, Part II
A Study of a Gravity-Gradient-Stabilized Nimbus Spacecraft Final Study Report, Jul. - Dec. 1965
An Active and/or Passive Spacecraft Attitude Control
Magnetometers and Solar Sensors as Attitude Indicators for Rockets and Satellites
Feasibility Study of an Aeronomy Satellite Final Report
Large Astronomical Satellite Space Reference System
Spacecraft Technology. Vol. Ii - Control and Stabilisation
Outline of Computer Simulation for the Control System of the L.A.S
A Possible Attitude Control System for the L.A.S
Large Astronomical Satellite. Fine Attitude Control
Impulse and Thrust Test of a Sublimating-Solid Micropropulsion System
Assessment of the Performance of the Eldo First Program Attitude Reference Unit in an Inertial Role
Project Eloise - Proposal for a European Large Orbiting Instrumentation for Solar Experiments
Position Determination of a Stationary TV Communications Satellite with Horizon Sensors
Analysis and Design of Space Vehicle Flight Control Systems. Volume XII - Attitude Control in Space
Satellite Attitude Control System, Using Integrating Gyros as Torquers
Control and Stabilisation of Spacecraft. Volume 1 - Introduction and Seminars
On the Application of Electric Propulsion to Satellite Orbit Adjustment and Station Keeping
Computer Program on Attitude Perturbations and Magnetic Control of a Spin-Stabilized Satellite
Simplified Processing of Star Tracker Commands for Satellite Attitude Control
Stability Criteria for the Oao Coarse Pointing Mode, Part 1 Final Report
Evaluation of an Ion Propulsion System for a Synchronous Spacecraft Mission
Facilities for Simulating Attitude Motion of Spacecraft
Application of Magnetic Torquing for Desaturation of Control Moment Gyros in Space Vehicle Control
Attitude Control System of the Eldo-Pas Satellite Final Report
Attitude Stability of a Spinning Passive Orbiting Satellite
Launch and Space Vehicle Control Studies. Volume 2 - Space Vehicle Control Studies Final Report