Add to ORKGThe application of a single movable mass to generate control torques for the attitude control of space vehicles is discussed. The feasibility of a movable mass control in stabilizing a cable-connected, artificial gravity configuration is proposed. A dynamic model for cable-connected configurations to account for the aggregate motion of the space station and relative torsional motion between the crew quarters and counter weight is developed
Spacecraft attitude control with strapdown inertial reference system and onboard digital compute
Operational and structural design criteria for artificial gravity stabilization of rotating space st...
Self adaptive control techniques for attitude control on Saturn 5 launch vehicle
Aspects of an attitude control system were studied and developed for a large space base that is stru...
Design and operation of attitude stabilization and control system for Biosatellit
Attitude control techniques for the pointing and stabilization of very large, inherently flexible sp...
Momentum management is discussed for a Large Space Structure (LSS) with the structure selected confi...
Studies of human orientation and manual control in high order systems are summarized. Data cover tec...
The augmentation of structural characteristics, mass, damping, and stiffness through the use of cont...
Simulation of stabilization and control for spinning, manned space station to provide artificial gra...
A theoretical development and associated digital computer program system is presented. The dynamic s...
An internal autonomous control system to either completely detumble a spacecraft or lessen the tumbl...
Research efforts on various methods that employ moving external parts for spacecraft control are pre...
The use of a movable mass control system to stabilize an arbitrarily tumbling asymmetric vehicle abo...
A study was made, leading to development and analysis of a technique allowing the control moment gyr...
Spacecraft attitude control with strapdown inertial reference system and onboard digital compute
Operational and structural design criteria for artificial gravity stabilization of rotating space st...
Self adaptive control techniques for attitude control on Saturn 5 launch vehicle
Aspects of an attitude control system were studied and developed for a large space base that is stru...
Design and operation of attitude stabilization and control system for Biosatellit
Attitude control techniques for the pointing and stabilization of very large, inherently flexible sp...
Momentum management is discussed for a Large Space Structure (LSS) with the structure selected confi...
Studies of human orientation and manual control in high order systems are summarized. Data cover tec...
The augmentation of structural characteristics, mass, damping, and stiffness through the use of cont...
Simulation of stabilization and control for spinning, manned space station to provide artificial gra...
A theoretical development and associated digital computer program system is presented. The dynamic s...
An internal autonomous control system to either completely detumble a spacecraft or lessen the tumbl...
Research efforts on various methods that employ moving external parts for spacecraft control are pre...
The use of a movable mass control system to stabilize an arbitrarily tumbling asymmetric vehicle abo...
A study was made, leading to development and analysis of a technique allowing the control moment gyr...
Spacecraft attitude control with strapdown inertial reference system and onboard digital compute
Operational and structural design criteria for artificial gravity stabilization of rotating space st...
Self adaptive control techniques for attitude control on Saturn 5 launch vehicle