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Numerical Computing for Ensuring the Trajectory Control of Aerospace Vehicles

Yury Lazarev
A numerical method is under consideration based on the sequential linearization and used to provide the multi-channel control and monitoring, both nominal and commanding, of the aerospace vehicles trajectories. The procedures of the functional differentiation, finite-dimensional approximation, making allowance for the constraints for guidance and motion regimes are described, as well as the methods for the nominal and commanding control.
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