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Closed-form error probabilities are derived to verify the simulations.
Control strategies are derived to accomplish the task.
Fuzzy decision factors are derived to isolate faults.
Steady closure equations are derived to calculate the dispersion tensor.
Equations are derived to describe the integrated aircraft-active system.
Closed form expressions are derived to characterize these response fluctuations.
In addition, optimal cancelation signals are derived to minimize the total power of sidelobes.
Cramer-Rao bounds (CRB) are derived to obtain more insights of this scheme.
Then, successive orthogonal gradient vectors are derived to form a basis of the signal subspace.
Therefore, linear equations are derived to relate aquifer and geophysical parameters in the present study.
Thanks to the especial character, a few approaches are derived to eliminate the error e(n).
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