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Simulation results demonstrate the effectiveness of the proposed attitude controller.
Finally, simulation results are presented to illustrate the effectiveness of the proposed attitude control approaches.
Simulation results are provided to demonstrate the effectiveness of the proposed attitude tracking control algorithm.
Numerical simulations are presented to show the effectiveness of the proposed attitude tracking approach.
Numerical simulations are presented to show the effectiveness of the proposed attitude synchronization and tracking approaches.
Performance of the proposed attitude control subsystem is demonstrated by numerical simulations.
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The proposed attitude-based models are valid for arbitrary wheel terrain geometry and can lead to control purpose directly.
After proposing a new class of robust attitude control laws for the three-axis attitude stabilization of spacecraft with inertia uncertainties, it is shown that the proposed robust attitude control laws are optimal with respect to performance indices.
The rest of the manuscript is organized as follows: the proposed cascade attitude control strategy is first given in "The proposed cascade attitude control strategy" section.
A novel adaptive fuzzy gain-scheduling sliding mode control (AFGS-SMC) approach is proposed for attitude regulation of unmanned quadrotors.
Subsequently, a stability analysis is presented to verify the performance of the overall proposed cascade attitude control approach.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com