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The maneuvering problem involves two tasks.
The output maneuvering problem involves two tasks.
In particular, we stress that for a complex mobile multi-link robotic structure such as a snake robot, formulating a pure path following, trajectory tracking, or maneuvering problem is unusual (for definitions of these problem formulations, see [27]).
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Control theory has long been applied to maneuvering problems and at present this trend is continuing at an increased rate.
The rotating beam spin-up maneuver problem is solved.
These concepts will be applied in Section 7 to analyze the pull-up maneuver problem.
The proposed method is then applied to an operational target phasing maneuver problem.
For this reason, we apply the above algorithm as well to the maneuver problem of the upper stages of the launch vehicles.
In this section, we address the minimum time-energy pull-up maneuver problem for airborne launch vehicles with a focus on the numerical solution method.
end{aligned} The optimal pull-up maneuver problem ((mathcal {P}_{A})) consists in steering the bi-input control-affine system (31) from x 0)=x_{0} (32).
Duration of mission, set of stages, maneuvers, problem of approaching and landings on Phobos have been reflected in problems of mechanics and motion control of the SC.
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