The influence research of constraints on possibility of two-channel control by aerospace vehicles suborbital trajectories

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The influence of constraints on character of suborbital trajectories of aerospace vehicle and type of control dependences is investigated. A result over of the numeral forming of two-channel control by suborbital trajectories at presence of constraints for guidance and motion regimes is considered.

Aerospace vehicle, suborbital trajectory, two-channel control, sequential linearization, numerical simulation

Короткий адрес: https://sciup.org/148203516

IDR: 148203516

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