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Basing on the linearized model, we derive an analytical expression of a constrained controlled Poincaré map.
Inspired by Fitts' information channel model, we derive a measure of instantaneous motor throughput.
From this nonlinear model, we derive a linearized state space model for the spacecraft system.
In our average-case model, we derive optimal functions under neutral (or impartial culture) probabilistic models.
To create this model, we derive entity information throughout the entire life cycle flow by using life cycle simulation technique.
From this model we derive an irrational transfer function to design a stabilizing boundary control in the frequency domain.
Based on the model, we derive an analytical solution for the dynamic DE under homogeneous in-plane deformation.
Using the four-band continuum model we derive a general expression for the infinite-mass boundary condition in bilayer graphene.
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This characterization is used as a baseline for the projection model we derived in next section.
For an LTE-A uplink transmission model, we derived SINR expressions, both with and without DFT pre-spreading.
For this noise model, we derived both exact and approximate formulas for the bias function and the noise variance function, taking clipping of the dynamic range into account.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com