Add to ORKGExperimental simulation on on-off reaction jet damping and attitude control system for spinning bod
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
Six subjects successfully reorinted the attitude of a simulated remote maneuvering unit (RMU) using ...
In-flight simulation to evaluate simultaneous use of attitude control for jet VTOL maneuverin
Automatic attitude control system test for satellite using inertia wheels mounted on air bearing
The mission requirements for some satellites require that they spin continuously and at the same tim...
Results are presented of experimental investigation of the controlled and uncontrolled dynamical beh...
An executive summary and an analysis of the results are discussed. A user's guide for the digital co...
Attitude reacquisition of gravity gradient control moment gyro stabilized spacecraf
Impulsive or time-decaying disturbances of sufficient magnitude will cause a gravitygradient control...
Attitude stabilization of manned spacecraft by twin gyros and pulse-modulated reaction jet
Feasibility of using fixed simulator to determine stall and spin characteristics of fighter aircraf
Abstract: The off-optimum situation on the spacecraft, equipped with reaction wheels, is t...
The air-bearing spin facility was developed to determine experimentally the effect of energy dissipa...
A theoretical study was made of the angular motions of spinning bodies in space. The analysis was ba...
This thesis models the motion of the NPS satellite ORION using the three Euler rotation angles. The...
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
Six subjects successfully reorinted the attitude of a simulated remote maneuvering unit (RMU) using ...
In-flight simulation to evaluate simultaneous use of attitude control for jet VTOL maneuverin
Automatic attitude control system test for satellite using inertia wheels mounted on air bearing
The mission requirements for some satellites require that they spin continuously and at the same tim...
Results are presented of experimental investigation of the controlled and uncontrolled dynamical beh...
An executive summary and an analysis of the results are discussed. A user's guide for the digital co...
Attitude reacquisition of gravity gradient control moment gyro stabilized spacecraf
Impulsive or time-decaying disturbances of sufficient magnitude will cause a gravitygradient control...
Attitude stabilization of manned spacecraft by twin gyros and pulse-modulated reaction jet
Feasibility of using fixed simulator to determine stall and spin characteristics of fighter aircraf
Abstract: The off-optimum situation on the spacecraft, equipped with reaction wheels, is t...
The air-bearing spin facility was developed to determine experimentally the effect of energy dissipa...
A theoretical study was made of the angular motions of spinning bodies in space. The analysis was ba...
This thesis models the motion of the NPS satellite ORION using the three Euler rotation angles. The...
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
Six subjects successfully reorinted the attitude of a simulated remote maneuvering unit (RMU) using ...
In-flight simulation to evaluate simultaneous use of attitude control for jet VTOL maneuverin