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Spin
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stabilization
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Attitude Determination of Spin Stabilized Spacecraft Using a Digital Aspect Sensor
Pendulum-Type Nutation Damper Used in the NASA Atmospheric Structure Satellite, S-6
Guidance and Control of a Man-Portable Precision Munition Concept
Attitude determination of spin stabilized spacecraft using a digital aspect sensor
Some design considerations for spin-stabilized satellites with rigid expandable structures
Passive Stabilization of Rotating Spacecraft Using Dynamic Fluid-Pressure Equilibrium
Pendulum-type nutation damper used in the nasa atmospheric structure satellite, s-6
Sss-a Etu Attitude and Spin Control Subsystem Magnetic Tests
Attitude Perturbations and Magnetic Control of a Spin-Stabilized Satellite, Part II
Spacecraft Attitude Stabilization Systems
Trajectory Prediction of Spin-Stabilized Projectiles With a Steady Liquid Payload
Attitude Stabilization of Satellites in Orbit
A digital system for accurate time sector division of a spin stabilized vehicle
Spin-Tunnel Investigation of a 1/13-Scale Model of the NASA AD-1 Oblique-Wing Research Aircraft
Techniques for Earth-Pointing Attitude Control of a Spacecraft
Techniques for Earth-Pointing Attitude Control of a Spacecraft
Nutation Control During Precession of a Spin-Stabilized Spacecraft
Nutational Stability of Multi-Body Spine- Stabilized Satellites
Country Plans Three-Axis Weather Satellite. Abstract Only
Computer Program on Attitude Perturbations and Magnetic Control of a Spin-Stabilized Satellite
An Automatic Attitude Control System for a Spinning Satellite - a Theoretical Assessment
Evaluation of the Kellett Gyratory Stabilizer Installed on the H-21 Helicopter
Effect of Inertia Properties on Attitude Stability of Nonrigid Spin-Stabilized Spacecraft
Attitude Perturbations of a Spin-Stabilised Satellite on a Highly Eccentric Orbit
Attitude Ground System (AGS) for the Magnetospheric Multi-Scale (MMS) Mission
Nutation Control During Precession of a Spin-Stabilized Spacecraft
Control and Stabilization of ESA (European Space Agency) Satellites
Deployment Mechanism for the Space Technology 5 Micro Satellite
Evolution of Spacecraft Design Methods as a Function of Environmental and Geometrical Constraints
Advanced Technological Satellite Electro-Mechanical Despun Antenna Final Report
Attitude Reorientation of Spacecraft by Means of Impulse Coning
Attitude stability of a spinning passive orbiting satellite
Attitude Stability of a Class of Partially Flexible Spinning Satellites
Spacecraft Attitude Determination Accuracy from Mission Experience
Multiple Attitude Maneuvers for a Spinning Spacecraft Disturbed by Solar Radiation
Attitude Stability of Spinning Satellites
Attitude Determination for the Satellite ESRO 2. Part 1 - Principles
Method of Controlling the Spin Rate of Tube Launched Rockets