The phrase "attitude control device" is correct and usable in written English.
It can be used in contexts related to engineering, aerospace, or robotics, where it refers to a mechanism that manages the orientation of an object in space.
Example: "The spacecraft is equipped with an advanced attitude control device to maintain its stability during flight."
Alternatives: "orientation control system" or "stability control mechanism".
The analytical analysis of the advantages of the proposed mechanism over the existing inertial attitude control devices are introduced.
Internal actuators, such as moving mass actuators and reaction wheels, have been proposed as attitude control devices for autonomous underwater vehicles.
To precisely control and stabilize ExoPlanetSat, Draper and MIT researchers built custom avionics and off-the-shelf reaction wheels, a type of mechanical device used for attitude control, at the base of the spacecraft to maneuver it into position.
The particular memory device used in the attitude control system of the Tracking and Data Relay System (TDRS-1) lends itself to the study of this phenomena due to its high susceptibility to such upsets.
Electrochromic devices have been used for the attitude control of a spinning solar sail in a deep space mission by modulating the reflectivity of the sail membrane.
Control moment gyros (CMGs) are a widely used device for generating control torques for spacecraft attitude control without expending propellant.
With respect to spacecraft attitude control, reaction spheres are promising alternatives to conventional momentum exchange devices for the benefits brought by their 4π rotation.
In the mission, a reflectivity control device was employed to generate a torque to control the attitude of the sail effectively.
He used a small bungee cord exercise device for "a little bit of stretching", before dropping into manual attitude control, where he reported a sudden burst of oversteering and high fuel use.
Synchronous vibration can be caused by rotor imbalance in high-speed rotors of momentum exchange devices, and the imbalance vibration is the main disturbance for attitude control of spacecrafts.
