"maneuver control" is a correct and usable phrase in written English.
It is often used in science, engineering, or military contexts to refer to the act of directing or controlling the movements of something. For example, "The platoon was able to take cover thanks to the skillful maneuver control of the captain."
According to the numerical simulation results it can be concluded that the proposed hybrid controller has a suitable and efficient performance for maneuver control and suppressing the transverse vibrations of the structure.
In order to further improve the interception capability, it constructs maneuver control model through adding maneuver control item to the guidance law.
This paper presents a slew maneuver control design of three-axis rotational flexible spacecraft.
This paper deals with maneuver control and vibration suppression of a two-link flexible arm with embedded smart materials.
For the spacecraft with flexible appendages, CSVS based on zero-placement is used to design the time optimal large angle maneuver control strategy.
This paper presents a dual-stage control system design method for the rotational maneuver control and vibration stabilization of a flexible spacecraft.
The controller consists of a variable structure control (VSC) for maneuvering control of the slow subsystem and a Lyapunov based controller for vibration suppression of the flexible structure.
For reorientation maneuvers, control moment gyros are utilized with a well-known singularity problem described in this work investigated by predicting one-step ahead singularity index.
A fault tolerant control (FTC) design technique against actuator stuck faults is investigated using integral-type sliding mode control (ISMC) with application to spacecraft attitude maneuvering control system.
An optimization process, which attempts to obtain vehicle maneuvering control parameters to minimize the overall crash risk, is integrated into the proposed evaluation framework.
This paper presents a dual-stage control system design method for the flexible spacecraft attitude maneuvering control by use of on off thrusters and active vibration control by input shaper.
